Space Sunday: major Artemis updates and a rollback

Credit: NASA

Yes, there’s been a lot in this column about Project Artemis and the US-led programme to return humans to the Moon, and while it might make Space Sunday sound a bit like a scratched record (Artemis..,Artemis…Artemis…), there is good reason for this: there’s a lot of news about the entire programme, from the anticipated launch of Artemis 2 and its crew on a trip around the Moon and back, to the focus of the main part of this article: major changes to the Artemis programme as a whole; so bear with me!

NASA’s current Administrator, Jared Isaacman, continues to surprise and impress despite concerns over his non-NASA activities and involvement with favoured space contractors. In my previous Space Sunday article, I covered Isaacman’s direct and open approach to the problems endemic to the Boeing CST-100 Starliner programme, and to the core of NASA’s management responsible for managing it (with two of the most senior resigning in the aftermath).

Following the press conference on that matter – which included the reading out of a letter to all NASA staff-  Isaacman was present at a February 27th, 2026 Project Artemis update which carried its own surprises whilst signalling a change in direction for the programme – potentially putting it on a far better footing that had previously been the case.

The update saw a number of significant announcements:

  • The much-criticised Space Launch System (SLS) is not to be cancelled as yet – something many outside NASA have called for, despite there being no currently-available launch vehicle that can match its capabilities (see: Space Sunday: of Artemis and Administrators).
  • However, SLS will be changing, with one significant element – the Exploration Upper Stage – now cancelled.
  • As a result of the Exploration Upper Stage cancellation, the Block 1B variant of SLS will no longer be part of the SLS enhancement programme, nor, potentially, will be the even more powerful Block 2 version.
  • NASA will attempt to raise the launch cadence for SLS from approximately once every 3 years to once every 10 months.
  • Artemis 3 is no longer a lunar landing mission, but will be an Earth-orbiting test flight involving at least Human Landing System vehicle.
  • The original Artemis 3 lunar landing mission is therefore redesignated Artemis 4, but the time frame remains a (optimistic) 2028.

SLS Changes

Much of the critique surrounding SLS has been on the matter of launch cost, which stands at some US $2.5 billion per vehicle. However, these costs are based on the overall development of SLS and Orion, and are not simply the physical cost of get a specific launch stack off the pad. This is something many of the louder voices raised against SLS – notably those from the SpaceX corner – tend to ignore when pointing to the “lower” cost of something like Starship, which is put at around US $100 million per launch. In this, it needs to be pointed out that this has yet to be proven, as Starship has yet to actually achieve orbit, and even then, launch costs for NASA could be as much as US 1.3 billion, when all of the required tanker launches and the launch of the (also unproven) orbital propellant station the Starship HLS will require just to get itself to the Moon.

That said, SLS is a costly launch mechanism; in 2023, the US Government Accountability Office (GAO) issued a report stating SLS was “unsustainable” at current spending levels, and suggested that launch costs could increase over time to as much as US $4 billion as a result of the technical complexity of the system, plans to try to extend its capabilities and its low launch cadence.

Exploration Upper Stage and “Near Block 1” SLS Development

Dropping the Exploration Upper Stage (EUS) from the SLS development curve should address some of these concerns over rising costs.

EUS was due to debut with the Block 1B development of SLS, providing it with a more powerful and capable upper stage than the current Interim Cryogenic Propulsion (ICPS) upper stage. As it is now cancelled, NASA is pivoting away from the Block 1B version of SLS in order to develop a “near Block 1” upgrade, which will use a new upper stage in place of both ICPS and EUS.

The original planned evolution of SLS, from the current Block 1 version for crewed launches through a cargo variant of the same vehicle to the Block 1B version utilising the EUS in both crewed and cargo versions, through the evolved Block 3 design with more powerful solid rocket boosters. Under the new plan, NASA will replace the Block 1B version with a “near Block 1” enhanced variant. Credit: NASA

Just how much this will save is open to debate: some US $3 billion has already be spent in developing EUS, and there will obviously be costs involved in developing a commercially-based replacement for it and ICPS. But there are other another compelling reasons for replacing EUS with a unit more in line (if more powerful) than the ICPS: simplicity of overall design and design and continuity of experience.

The Block 1 SLS is now a known creature, foibles and issues all taken as read. It’s a vehicle NASA is continually gaining knowledge and understanding in operating. Block 1B, with the EUS, it’s extended core stage elements (extended interstage and the enlarged universal stage adaptor) is a different beats, liable to demonstrate different flight characteristics and dynamics as well as introducing new elements which could have their own teething problems. Sticking with an only slightly modified vehicle to supersede the current Block 1 vehicle, reduces many of these factors, allowing NASA to “standardise” the SLS design and continue to gain data, knowledge and understanding on  / of its characteristics incrementally. This was pretty much how things were handled back in the Apollo era, and the approach has a lot going for it, a point acknowledged during the briefing.

After successful completion of the Artemis I flight test, the upcoming Artemis II flight test, and the new, more robust test approach to Artemis III, it is needlessly complicated to alter the configuration of the SLS and Orion stack to undertake subsequent Artemis missions. There is too much learning left on the table and too much development and production risk in front of us. Instead, we want to keep testing like we fly and have flown. We are looking back to the wisdom of the folks that designed Apollo. The entire sequence of Artemis flights needs to represent a step-by-step build-up of capability,

– NASA Associate Administrator Amit Kshatriya

Exactly who will provide the replacement for ICPS / EUS and what form it will take was now discussed at the briefing. However, it was made clear that all of NASA’s contractors and partners in Artemis were consulted through the driver to redirect the programme, and all have been supportive of the moves – even Boeing, who stand to lose the most with the EUS cancellation, whilst SpaceX and Blue Moon have both opted to “accelerate” the development of their HLS systems.

Perhaps two of the strongest potential contenders for producing a new upper stage for SLS are United Launch Alliance (ULA) and Blue Origin.

ULA already has the powerful cryogenic Centaur V upper stage. Centaur is a venerable launch vehicle stage with a lot of expertise behind it, with the Centaur 5 already forming the upper stage of ULA’s Vulcan-Centaur rocket. Blue Origin, meanwhile, has the upper stage of their New Glenn booster. Whilst a “new kid on the block”, the stage has already proven itself reliable on two high-profile flights for New Glenn, and will shortly be back in action for a third flight, thus experience is quickly being gained in its operation. Further, blue Origin are already looking to develop an enhanced version of the stage in line with their plans for an even more powerful variant of their New Glenn vehicle, thus there is potential here as well.

Neither Centaur V nor the New Glenn upper stage would be suitable for SLS straight off the shelf, but using them as either a basis for a new stage design or developing a variant off of an existing design (Blue Origin) could significantly reduce the costs and time involved in developing and testing a new SLS stage.

Launch Cadence

Another mitigating factor when it comes to reducing overall costs is the decision to try to launch SLS on a greater cadence than has thus far been seen. Isaacman would specifically like to see an SLS / Artemis launch once every 10 months, putting Artemis almost on a similar launch cadence as Apollo. Doing so will likely increase Artemis costs, but it also brings some very clear benefits:

  • Personnel expertise. Gaps measured in years between launches can result in personnel expertise loss as people become tired of waiting for the next launch and seek a career move elsewhere, taking their expertise with them. A faster launch cadence with clear mission objectives is more likely to keep more of that expertise in-house at NASA for longer.
  • It makes Artemis potentially more robust, presenting NASA with a chance to present a clear roadmap for achieving the goals of establishing a lunar base and maintaining a human presence there. Clear time frames and mission objectives also help Congress in allowing the money to flow into NASA to support the programme.

Of course, achieving such a cadence is no easy task; thus far, Artemis 1 and Artemis 2 (of which more below) have demonstrated that, like it or not, SLS and its ground support systems are extremely complex and subject to technical issues which can so easily upset launches.

Artemis 3 – No Longer Aiming for the Moon

The decision to “divert” Artemis 3 to an Earth orbital mission was perhaps the biggest surprise in the update – although “divert” is not entirely correct.

What is proposed is the insertion of an additional Artemis / SLS launch between what is currently Artemis 2 and what would have been Artemis 3, the first crewed lunar landing in the programme. That mission – presumably utilising the same crew – will now effectively become Artemis 4, with the new Earth-orbital mission taking the name Artemis 3.

An infographic outlining the revised Artemis missions (2 through 6), with the Artemis 2 crewed mission around the Moon and back (2026) at the top; the new Artemis 3 mission (2027) centre and the first three crewed lunar landing missions (Artemis 4 through 6). Credit NASA
The aims of the revised Artemis 3 mission – scheduled for a 2027 launch – so far comprise (additional mission goals may be added as the mission requirements are further assessed):

  • On-orbit rendezvous and docking with one or other (or possibly both) of the current Human Landing System vehicles in development: Blue Origin’s Blue Moon Mark 2, and the nascent SpaceX  Starship-derived HLS.
  • Perform integrated checkout of life support, communications, and propulsion systems on both HLS vehicles and assess their suitability / practically for zero gravity operations.
  • Carry out comprehensive tests of the new extended extravehicular activity (xEVA) suits to be used both with Artemis as as a replacement for the current generation of US EVA suits on the International Space Station.

This is actually a smart step on NASA’s part, and harkens back to the Apollo era and specifically, the Apollo 9 mission.

Artemis 3 will focus on earth-orbit rendezvous with either Blue Origin’s Blue Moon Mark 2 HLS or the SpaceX Starship HLS (depending on which is available at the time) or both (if both prove to be ready for testing – which right now looks unlikely in the case of the SpaceX HLS). Credit: NASA

Under the original Artemis plan, no provision was made for any on-orbit human testing of the SpaceX HLS vehicle ahead of Artemis 3. Instead, SpaceX were obliged to send and uncrewed HLS lander to the Moon and conducted an automated landing (or possibly 2) – but there were no provisions for any crewed testing of the vehicle prior to Artemis 3.

Conversely, Blue Moon Mark 2, with its longer lead time (not being required – in theory – until Artemis 5 under the previous plans, and now Artemis 6 under the revised approach) would have undergone Earth orbit crewed testing prior to being used for lunar operations.

As such, this new step offers a means by which both vehicles (assuming both are ready for a 2027 launch) can be properly tested in Earth orbit, where the risks to the crew are potentially reduced, simply because they can use Orion to make a fast return to Earth. Thus, both can be properly assessed, including any shortfalls they might exhibit in advance of any attempt at a lunar landing. This is something that is clearly much better for all concerned than otherwise sitting and crossing fingers, as would have been the case with the original Artemis 3 mission.

Other Changes

Additionally, the Artemis Update indicates further changes within NASA’s operating structure as a whole with a drive to rebuild core competences and to better oversee commercial contracts and be more hand-on with commercial partners (as indicated in the Starliner press briefing). Key to this will be the implementation of standard processes right  across the space agency, not just covering Artemis, but all commercial partnership and space projects.

Further, the space agency will embark on a process of new and more extensive involvement with Congress to keep them appraised of progress with SLS and Artemis, and has already embarked on a restructured process of negotiating with commercial partners and engaging them in NASA’s decision-making processes.

Whilst nothing should be definitively drawn from it, it is somewhat interesting that the new SLS upper stage designed to replace both ICPS and EUS (seen in the centre, above, with Orion attached) has a marked similarity to the New Glenn upper stage, seen to the right Orion and powering the Blue Moon Lander Mark 2 to orbit.

In the meantime, the NASA announcement has received a largely positive reaction from observers and stakeholders, and the approach it advocates potentially helps put Project Artemis on a much more realistic footing to achieve its goals.

Artemis 2 SLS Rolled Back to the VAB

As I reported in my previous Space Sunday update, Artemis 2 suffered another setback in plans to get a crewed Orion space vehicle on a 10-11 day free return flight to the Moon (with a day spent in a high Earth orbit beforehand) off the ground in March.

The Crawler-Transporter edges the Artemis 2 SLS stack and mobile launch platform into one of the two massive high bays of the VAB at Kennedy Space Centre near the end of an 11+ hour journey back from the launch pad. Credit: NASA livestream

The issue this time resides within the helium pressurisation system within the rocket’s Interim cryogenic Propulsion Stage (ICPS), which is required to get Orion to orbit and plays a role in meeting all of the mission’s planned goals. As I noted at the time of writing that update, NASA felt there were two potential routs to resolving the issue: by leaving SLS on the pad at Kennedy Space Centre’s Launch Complex 39B (LC-39B). Or rolling the entire stack back to the Vehicle Assembly Building (VAB), where a more comprehensive examination of the issue could be performed.

It was decided the latter was the better choice of action, and so on February 25th, 2026, the Artemis 2 launch vehicle and its Mobile Launch Platform were slowly and gently rolled back to the VAB atop one of the famous Crawler-Transporters.

A view from inside the VAB as Artemis 2 arrives. Note the curved gantries either side of the  upper parts of SLS. These can be extended outwards (as can other levels within the high bay) to encapsulate the rocket and provide ease of access to its vitals for engineers. Credit: Cameron (@nyoomtm)

The physical move of the rocket and its launch tower structure commenced at 14:38 UTC, and took over 11 hours to complete, the Crawler-Transporter inches the entire structure into one of the VAB’s massive high bays inch by inch with incredible precision given the overall size of the Crawler-Transporter and its payload. The night-time arrival also afforded some unique views of the entire stack edging up to and then entering the VAB.

Currently, the hope is to correct the helium pressure issue in time to get the rocket back to the pad so it can meet an April 1st through 6th (inclusive) launch window. However, more extensive rectifications to the helium system, if required, will be left for the next SLS vehicle which will carry the crew selected for the new Artemis 3 mission to orbit.

Space Sunday: Starliner and Artemis woes

An uncrewed CST-100 Starliner vehicle approaching the International Space Station during the vehicle’s Orbital Flight Test 2 mission, May 2022. Credit: NASA

Boeing’s CST-100 Starliner programme, designed to offer both NASA and commercial space companies with the means of delivering astronauts to low-Earth orbit space stations such as the International Space Station (ISS) and the Blue Origin / Sierra Space led consortium’s Orbital Reef station, has had a very chequered history with the number of issues far outweighing the number of successes.

On all three occasions the CST-100, comprising a capsule with a capacity for up to seven crew – although 4 plus a measure of cargo is liable to be the usual complement, together with a service module – has reached orbit, it has done so while encountering a series of issues / failures.  Indeed, such is the nature of some of the problems, they actually led to delays in getting the second flight test off the ground. More significantly, some of the issues were potentially known about as far back as June 2018. It was then, during a hot fire test of one of the vehicle’s RS-88 launch abort motors, when four of eight values on the vehicle’s propellant flow system failed, releasing 1.8 tonnes of highly toxic  monomethylhydrazine propellant and causing a fireball that engulfed the test rig.

The July 2018 hot fire test of an RS-88 launch escape motor used on Boeing’s Starliner. During the test 4 of eight valves failed, resulting in the dumping 1.8 tonnes of highly toxic propellants which in turn caused a fire which engulfed the engine and test stand. Credit: Boeing / Aerojet.

Whilst blaming engine supplier Aerojet Rocketdyne for the hot fire test incident, Boeing simultaneously sought to keep the news of the incident quiet, and limited the circulation of information relating to it to a few senor programme managers at NASA, who agreed to also keep the incident out of the public eye as much as possible so as not to further delay the programme, which was already behind schedule.

Although it is near impossible to state with certainty that this event market the start of successive failures of management both within Boeing and NASA as to how Starliner and its various issues and problems were both handled and communicated between the two parties, it fits with a pattern seen throughout the last several years of Starliner’s troubles.

All of this has now been made clear in a comprehensive report released by the new NASA Administrator, Jared Issacman, in the wake of an in-depth investigation covering several months into the Starliner project. Released during a public press briefing, the 311-page report (partially redacted) goes into extensive depth relating to the three Starliner flights to orbit to date: the uncrewed Orbital Flight Test 1 (OFT 1, 2019) and its follow-up Orbital Flight Test 2 (OFT 2, 2022), and the first Crew Flight Test (CFT 1, 2024) which famously resulted in heady reports of the mission crew – Sunita Williams and Barry Wilmore being “stranded” in space as if they were utterly helpless when in fact they are working aboard the ISS.

The report goes to great length to outline the core technical issues with Starliner relating to the four “doghouse” thruster packs mounted equidistantly around the circumference of Starliner’s service module and containing multiple large and small thrusters designed to provide the vehicle with flight motion and manoeuvring capabilities, together with the software issues which proved to be the undoing of the original OFT 1 mission which ultimately left the vehicle unable to rendezvous with the ISS and attempt an automated docking.

The Boeing CST-100 Starliner – A = crew capsule with major additional elements (1-9) comprising in order: the nosecone; parachute system cover; side hatch for ground-based access / egress; capsule RCS unit (x25 in total); landing airbags; heat shield; forward docking system port; 3x main parachutes; 3x windows. B = Service module with major additional elements (10 through 16) comprising in order: power and water, etc., umbilical connector to capsule; thermal control radiators for removing excess heat; “Doghouse” unit (x4), containing multiple RCS and OMAC thrusters each; monomethylhydrazine and nitrogen tetroxide propellant tanks; roll control RCS thruster (part of the Doghouse units); RS-88 launch escape engines; solar panels for electrical power. Credit: Boeing

But most startlingly, the report reclassifies the Crew Flight Test 1 as a Type A mishap. This is NASA’s most extreme rating for malfunctions aboard crew carrying vehicles; for example, both the Challenger and Columbia space shuttle losses were classified as Type A mishaps on account of the loss of all board both vehicles. Type A mishaps have several main criteria: Injuring or fatalities during flight; loss of a vehicle or its control; damage exceeding US $2 million.

At first glance, and given that a) Williams and Wilmore did manage to maintain control over their vehicle and make a successful docking with, and transfer to, the ISS; b) there were no injuries or fatalities; and c) US $2 million in damages is an exceedingly small amount in the scheme of things, reclassifying CFT 1 a Type A mishap might appear to be more a knee-jerk reaction than might be warranted. However, the events experienced during CFT 1 make it abundantly clear that designating it a Type A mishap should have occurred at the time  of the flight – or at least immediately afterwards as the situation was fully understood.

The key point here is the second criteria for specifying a Type A mishap: the loss of the vehicle or its control. During CFT 1’s approach to the ISS for rendezvous and docking, the vehicle suffered a critical failure of five thruster sets required for manoeuvring control ( in NASA parlance, the vehicle lost its required 6 degrees of freedom manoeuvring). Regardless of the fact that the crew regained the use of four of the thrusters units in short order and went on to complete a successful docking at the ISS, at the time the failure occurred, Starliner was effectively adrift, unable to correct its orientation or motion – or even safely back away from the ISS to avoid the risk of collision. In other words, loss of the vehicle’s control had occurred.

Nor, as it turns out, was this the only issue. During its re-entry and descent through the atmosphere, the Starliner capsule Calypso suffered a failure with one of its RCS thruster systems, resulting in a “zero fault tolerance” situation – meaning there was no back-up for the failed unit during what was a critical phase of the vehicle’s flight.

Boeing Starliner capsule Calypso sitting on its airbags at the at White Sands Missile Range in New Mexico, following its successful return to Earth at the end of the uncrewed Orbital Flight Test 1 in December 2019. Calypso was also the capsule used for the Crew Flight Test in 2024. Credit: Bill Ingalis

So why wasn’t CFT 1 designated a Type A mishap immediately after the fact? Here the report is uncompromising in its assessment: NASA managers overseeing the Starliner contract were more concerned with getting the vehicle certified for routine crew operations than with admitting it still has major flight qualification issues which should disbar it from routine use to launch crews. It is in this approach of directly pointing the finger and throwing back the covers on how NASA and its contract have been functioning within the Starliner contract that the report – despite the redactions within it – is uncompromisingly clear in apportioning blame.

In particular, the report highlights numerous issues with the way the contract – and by extension – all commercial partnership contracts are handled by NASA. Chief among these is that, whilst charged with overall oversight responsibilities for such programmes, NASA took an almost completely hands-off approach to Starliner, bowing to Boeing when it came to most critical decision making on the overall fitness  for purpose of the system. Challenges to internal decision making at Boeing were muted or non-existent, and when it was felt Boeing were obfuscating or failing to be properly transparent, NASA tended not to challenge, but simply started mistrusting their contractor, allowing further breakdowns in communications to occur.

For its part, Boeing felt it could compartmentalise issues into individual fault chains and fixes, rather than seeing and reporting them as they were, a series of interconnected chains of design issues, faults and upsets. As a result, issues were dealt with on a kind of patch-and-fix approach, rather than a systematic examination of chains of events and proper root cause analysis. In this, the report particularly highlights the fact that whilst Boeing has a robust Root Cause / Corrective Action (RCCA) process, all too often it was never fully deployed in dealing with issues, the priority being to find a fix for each issue in turn and move on in the belief things would be rectified once all the fixes had been identified and implemented.

A time lapse photograph of the Boeing CST-100 Starliner featuring the capsule Calypso, docked at the ISS in June 2024 during Crew Flight Test 1, which saw a further series of thruster issues for the vehicle, ultimately leading it to make an uncrewed return to Earth. Credit: NASA

The report goes into a number of recommendations as to how NASA must handle future commercial partnerships such as the Commercial Crew Programme (CCP) of which SpaceX and Boeing are both a part, and how it should exercise full and proper oversight and lose its hands-off attitude. Time will tell in how these changes will affect such contracts – not just with Boeing and CST-100, but also with the likes of SpaceX and the development of their lunar lander, a project where NASA has again been decidedly hands-off in it approach to the work, allowing SpaceX to continually miss deadlines, fail to produce vehicle elements in time for testing, and to seemingly pushed vehicle development to one side in favour of pursuing its own goals whilst still taking NASA financing to the tune of US $4.9 billion.

In respect of Starline itself, the root cause(s) of the thruster issues on the vehicle still has/have yet to be fully determined. However, Issacman has made it clear NASA will not be withdrawing from the contract with Boeing; instead he has committed NASA to refusing to flying any crew aboard Starliner until such time as Boeing can – with NASA’s assistance – demonstrate that the issues plaguing the vehicle have been fully understood and dealt with properly and fully.

Whether that can be done within the next 5 years of ISS operational life remains to be seen.

Artemis 2: WDR Success; Launch Again Delayed

The Artemis 2 Space Launch System (SLS) rocket successfully completed its pre-flight wet dress rehearsal (WDR) test on Thursday, February 19th, 2026, potentially clearing the path for a mission launch in early March – or at least, that was the hope.

As I’ve noted in recent Space Sunday updates, the WDR is a major test of all the ground systems associated with launching an SLS rocket, together with the on-board systems and all ground support personnel  to make sure all systems are ready for an actual launch and staff are up-to-speed with all procedures and possible causes for delays, etc. Such tests run through until just before engine ignition, and include fully fuelling the booster’s core stage with liquid oxygen and liquid hydrogen.

The WDR had previously revealed issues with the propellant loading system at the base of the mobile launch platform on which the rocket stands ahead of lift-off, with various leaks being noted the both the first Artemis 2 WDR and previously with the uncrewed Artemis 1 mission of 2022.

A ground level view of the Artemis 2 SLS sitting atop its mobile launch platform at LC-39B, Kennedy Space Centre, Florida. Credit: NASA/Ben Smegelsky

The original Artemis 2 WDR suffered issues with the liquid hydrogen feed into the rocket and with a filter designed to keep impurities out of the propellants. Both the problem valves and the filter were swapped-out ahead of the second WDR together with the replacement of a number of seals which showed minor signs or wear. Following the second WDR test, an initial review of the gathered data was performed, and the results gave NASA managers the confidence to officially name March 6th, 2026 as the target launch date for the mission, marking the opening of a 5-day launch window in March, with a further window available in April.

However, within 24 hours of the target launch date being announced, NASA was forced to issue a further mission postponement when another issue was discovered – this time a helium leak in the booster’s upper stage.

The new leak is entirely unrelated to those within the umbilical propellant system on the mobile launch platform and lies within the Interim Cryogenic Propulsion Stage (ICPS) pressurisation system.

The latest issue with the Artemis 2 SLS lies within the Interim Cryogenic Propulsion Stage (ICPS), aka the rocket’s upper stage, seen above, which will perform a number of tasks in the mission – including getting the Orion crew vehicle to orbit in the first place. The issues are entirely unrelated to those seen with the main propellant loading system at the base of the rocket. Image credit: United Launch Alliance.

The ICPS plays a critical role in both lifting the Orion vehicle to its initial orbit following separation from the booster’s core stage, and then moving it to a high altitude orbit prior to it and Orion entering a trans-lunar injection orbit, where – after the ICPS has separated from Orion, it will be used as a target for a series of planned rendezvous and simulated docking exercises to test Orion’s ability to carry out the precise manoeuvring required to dock with Moon-orbiting Moon landers and (eventually)with the Gateway station.

However, in order to function optimally, the ICPS requires a  “solid” – that is a specific rate of flow and pressure for the helium. Fluctuations in the flow – such as caused by a leak – cannot be tolerated. This means that in order to fly, Artemis 2 requires the issue to be properly addressed. This is something that might be done whilst leaving the vehicle on the pad; however, it might require the vehicle to be rolled back to the Vehicle Assembly Building (VAB) to allow complete access to the ICPS. At the time of writing, engineers at NASA were still evaluating which option to take.

But one thing is clear – with just two weeks between the discovery of the issue and the opening of the March launch window, there is precious little time to fully investigate and rectify the issue. As such, NASA is now shifting its focus towards having the mission ready for lift-off in time to meet the April 2026 launch window.

Space Sunday: lunar ambitions: the real and the not-so-real

The core stage of China’s new Long March 10 (CZ-10A variant) booster uses a single motor to ease itself into the waters of the South China Sea to await recovery after a highly successful test flight. Credit: CCTV video footage

The current “race for the Moon” is turning into a hare-and-tortoise situation on several levels, including internationally. On the one hand, there is America’s (arguably over-complicated, thanks to NASA’s insistence on the use of cryogenic propulsion to get to / from the lunar surface) Artemis programme, which seems to race along in fits and bursts (and frequently slams itself into a wall of delay) and then there is China’s more conservative “latter-day Apollo” approach, which quietly plods along, racking up achievements and milestones whilst seeming to be technologically far behind US-led efforts.

As noted, China’s approach to reaching the Moon, is something of a harkening back to the days of Apollo in that it uses a relatively small-scale crewed vehicle for getting between Earth and the Moon, and a similarly small-scale lander. However, size isn’t everything, and both crew vehicle and lander (the latter of which has a cargo variant) would be more than capable in allowing China to establish a modest human presence on the Moon, just as their Tiangong space station, whilst barely 1/4 the size of the International Space Station, has allowed them to do the same in Earth orbit. It is also important to recognise it as part of an integrated, step-by-step lunar programme officially called the Chinese Lunar Exploration Programme (CLEP) and familiarly referenced as the Chang’e Project after the Chinese Goddess of the Moon, which has allowed China to develop both a greater understanding of operations on the Moon and in understanding the Moon itself.

The Chang’e project commenced over 20 years ago, and recorded its first successes in 2007 and 2010 with its Phase 1 orbital robotic missions. This was followed by the Phase II lander / rover missions (Chang’e 3 and Chang’e 4) in 2013 and 2018 respectively, and then the Phase III sample return mission of Chang’e 5 (2020).

Currently, the programme is in its fourth phase, an extensive study of the South Polar Region of the Moon in preparation for human landings, nominally targeting 2030. This phase of the programme has already seen the highly successful Chang’e 6 mission, the first to retrieve surface samples from the Moon’s far side, as well as deploying a rover there. 2026 will see Chang’e 7 launched, a high concept resource seeking mission comprising an orbiter, lander and “lunar flyer”, all geared to locate resources which can be utilised by future missions.

China’s Chang’e 6 mission, launched in May 2024, was the first Chinese mission to the far side of the Moon, and the first mission to ever return samples gathered from the lunar far side and return them to Earth (June 2024). In this image, Chang’e 6 is seen from the Jinchan mini-rover, which piggybacked a ride to the Moon with the lander. Credit: CNSA.

In 2028, the last of the Phase IV mission will launch. Chang’e 8 is intended to be a combination of in-situ resource utilisation (ISRU) test bed, demonstrating how local materials (water ice, regolith) can be used to produce structures on the Moon via advanced 3D printing, and to establish a small ecosystem experiment in advance of human landings.

This approach means that from a standing start, China has replicated much of NASA’s work of the 1960s that helped pave the way for Apollo, but in much greater depth. It’s not unfair to say that by retuning such a focused series of mission phases – notably Phase IV – China potentially will develop a greater spread of knowledge concerning the Moon’s South Polar Region than NASA.

At the same time, China has been developing the hardware required for the human side of the Chang’e Project. This primarily takes the form of their Mengzhou (“Dream Vessel”) reusable crewed vehicle, the Lanyue (“Embracing the Moon”) 2-stage lunar  lander / ascent vehicle and the Long March 10 semi-reusable heavy lift launch vehicle (HLLV) offering a very similar capability to Blue Origin’s New Glenn vehicle.

Mengzhou is being developed in two variants: a low Earth orbit (LEO) variant, designed to ferry crews to / from the Tiangong space station. The second is being developed expressly for lunar missions, offering an increased mission endurance capability. The first uncrewed orbital test-flight for the 14-tonne LEO version of Mengzhou is due to take place in 2026, the system having been going through progressive flight tests throughout the 2010 and early 2020s. If successful, it will pave the way for the vehicle to start operating on crewed flights to Tiangong alongside the current Shenzhou craft, which it will eventually replace.

Launch of the CZ-10A and Mengzhou test vehicles, February 11th, 2026. Credit: CCTV

On February 11th, 2026, a test article of the 21-tonne Mengzhou lunar vehicle completed a significant test atop the core reusable stage Long March 10 (Chinese designation CZ-10A) booster. This was a combined mission to test both the Mengzhou launch abort system (LAS) whilst under the rocket’s maximum dynamical pressure flight-regime, and also the booster’s ability to complete an ascent to its nominal stage separation altitude of 105 km, and then make a controlled descent and splashdown close to its recovery ship.

Following a successful launch, the combined vehicle climbed up to the period of “Max Q”, around 1 minute into a flight and wherein the maximum dynamic forces are being applied to the entire stack. The Mengzhou LAS successfully triggered, boosting the vehicle away from the Long March core stage at high speed. The Mengzhou capsule then separated from the LAS performed a splashdown downrange.

The Mengzhou LAS powers away from the CZ-10A corse stage, carrying the Mengzhou capsule with it, as would be required should a critical malfunction occur with the Long March 10 rocket. Credit: CCTV
The Long March 10 core stage then continued a powered ascent profile, performing engine shutdown at 105 km before simulating an upper stage separation followed by a post-separation manoeuvre. This saw the stage enter “glide” phase, using its aerodynamic fins to maintain its orientation.

During this “glide” phase (actually a controlled descent, the stage orienting itself to fall engines-first), the booster carried out an automated pre-cooling of its engines in readiness for re-use and raise the pressure within the propellant tanks to settle their contents in readiness for engine re-use.

Cameras on the booster capture the deployment of the SpaceX-like grid fins on the upper end of the stage, which help it to maintain the correct orientation during its descent back to Earth. Credit: CCTV

Roughly one minute before splashdown, several of the engines successfully re-lit in a braking manoeuvre to bleed off much of the stage’s velocity. These were quickly reduced to just 3 motors and then a single motor as the stage came to a near-hover before that motor shutdown allowed it to settle smoothly and vertically in the water just 200 metres abeam of its recovery ship.

As an aside, it is interesting to contrast reporting on this flight with media coverage of SpaceX Starship “integrated flight tests”. In the case of the latter, almost every flight has been reported as some kind of spectacular success, despite most of the flights blowing up, barely meeting their assigned goals, or simply re-treading ground already covered. By contrast, the Mengzhou / CZ-10A core stage test flight has largely been defined as a “small step” in China’s progress, with some emphasising the flight “not reaching orbit” – which it was never intended to do.

In reality, the entire flight was a complete success. Not only did it demonstrate the Mengzhou vehicle’s LAS fully capable of lifting the command module and crew clear of an ascending CZ-10A should the latter suffer a malfunction during the most dynamically active phase of it flight, it also further demonstrated the capsule’s parachute descent system and its ability to make a recoverable splashdown (Mengzhou is capable of both water and land-based touchdowns, being able to be equipped with either a floatation device or airbags prior to launch).

Another still from the video of the test flight, showing the booster entering the see and its proximity to the recovery vessel, just visible on the right of the image. Future tests will see the recovery vessel attempt to “catch” a returning booster directly using a “tether” system. Credit: CCTV

Further, the test demonstrated the CZ-10A core stage’s ability to undertake a return to Earth and splashdown (again, the booster is designed to both land on a recovery ship a-la Falcon 9 and New Glenn, or make a splashdown close enough to the recovery ship so it can then be recovered – direct returns to the recovery vessel will be a part of future tests). Finally, such was the accuracy of the guidance systems, the rocket splashed down just 200 metres from the recovery ship, as planned.

That said, it is true that all the core components of the crewed phase of the Chang’e project still have a way to go before China can send a crew to the Moon. But like the tortoise, their one-step-at-a-time / keep-it-simple approach could yet see them become the first nation to do so since 1972.

Why SpaceX is most likely “Shifting from Mars to the Moon”

Thirteen months ago, in an attempt to bolster his failing “Mars colony plan” (a totally unrealistic fever dream of sending a “Battlestar Galactica” scale feet of 1,000 Starship vehicles carrying 1 million people to Mars to establish a colony there), the SpaceX CEO declared “the Moon is a distraction” and Mars was the focus for his company.

Well, he’s had 13 months to forget all that, as on the weekend of February 7th and  8th, 2026, the self-styled man who “knows more about manufacturing than anyone else alive on Earth” and yet cannot deliver on a single one of his manufacturing promises, declared that the Moon is now the focus of SpaceX’s endeavours, all as a part of a grand plan to “expand human consciousness and support his equally questionable idea of operating a 1-million strong constellation of Starlink satellites as a string of “data centres in space”. For good measure he mixes in terms such as “climbing the Kardashev scale” )the latter seems to be a particular reference point for so-called space entrepreneurs of late).

However, the real reason is liable to be far more mundane: the SpaceX CEO is again trying to justify the US $1.2 trillion valuation he and his fellow broad members arbitrarily awarded the company in January, and to justify such a figure in the face of an upcoming IPO whilst also possibly trying to further dazzle investors with shiny promises about orbital data centres and moon bases at a time when SpaceX has just “inherited”xAI and its cash burn-through of around US $1 billion a month.

The promise of a fully operational “Moon Base Alpha” (yes, once again we have a sci-fi trope to add gloss to an idea) in “10 years” will, undoubtedly go the same way as the more than a decade old claim that Tesla vehicles will be capable of full self driving “next year”; the statement that SpaceX would have Starship operational by 2022, and that Starship would fly around the Moon in 2023 and to Mars in 2024, err, 2026, err, 2028. That is to say, most likely never.

Martian Organics Cannot be Entirely Explained by Non-organic Processes

One of the major mysteries of Mars is the question of methane. It was first detected in more than faint trace amounts by the European Space Agency’s Mars Express mission in 2004. A decade later, NASA’s Mars Science Laboratory (MSL) rover Curiosity,  detected methane spikes and  organic molecules whilst exploring the floor of Gale Crater. Then in 2019, the rover a massive spike as it explored “Teal Ridge”, a formation of bedrock and deposits on “Mount Sharp” (Aeolis Mons).

Alongside of this is the vexing discovery of organic elements on Mars. These and the methane seem to point a finger towards the idea that the planet may have once harboured life. However, as even proponents of this idea point out, both organics and methane can result from purely inorganic interactions. The tick is – how to determine which might be the case.

An artist’s rendering of Curiosity at work in Gale Crater. Credit: NASA

In March 2025, Curiosity detected small amounts of decane, undecane, and dodecane in a rock sample, which constituted the largest organic compounds found on Mars to date. These offered the potential to determine which option might be more likely to cause their existence – organics or inorganic chemical reactions. All three are hydrocarbons could be fragments of fatty acids, also known as carboxylic acid.

On Earth, carboxylic acid (aka fatty acids) is a natural by-product of life. Such acid can be found in animal tissues, nuts and seeds. In the case of animal tissues, carboxylic acid is predominantly formed by the breakdown of carbohydrates by the liver and found within adipose tissue, and the mammary glands. however, they can also be created by inorganic reactions – such as lightning striking chemically rich soils (or regolith), hydrothermal interactions and photochemical reactions between ultraviolet radiation and hydrocarbon-rich mixtures.

In order to try to determine whether the fatty acids discovered by Curiosity preserved in ancient mudstone are the result of organic processes or inorganic. Whilst limited with working only with data from the rover’s Sample Analysis at Mars (SAM) spectrometer, the team sought to recreate the likely conditions on Mars some 80 million years ago – this being the amount of time the rock containing the acids would likely have been exposed to the surface atmosphere – and then work back from there to try to determine which would survive the longest: carboxylic acid produced by organic or inorganic means.

What they found was that organic mechanisms appear to leave far more in the way of organic remnants – such as decane, undecane, and dodecane – than the typical non-biological processes involved in forming carboxylic acid could produce. The team suggest that this might be because any organics responsible for the fatty acids might have been assisted by periodic impacts by carbonaceous meteorites, known to be sources of fatty acids formed in space.

A graphic shows the long-chain organic molecules decane, undecane, and dodecane, the largest organic molecules discovered on Mars to date. Credit: NASA/Dan Gallagher

However the team also urge caution: whilst their finding might move the needle further towards the idea that Mars once harboured life, they also clearly note that there is a need for greater study; Mars is a complex world, rich in complex interactions. As such, more and detailed study is required – preferably first-hand, through the obtaining of samples from Mars itself. Currently, and rather ironically, whilst NASA had planned to make samples from the Mars 2020 rover Perseverance available for return to Earth, these do not contain samples of a similar nature to those found by Curiosity.

More particularly, at the time Perseverance had launched to Mars with sample retrieval in mind, no-one had actually sorted out how such a retrieval might be achieved. As such, a series of highly complicated, overly expensive proposals were put forward, involving both US and European co-operation. Each of these were knocked down on the basis of complexity and escalating price – up to US $11 billion – or close to half of NASA’s overall budget – for such a mission was just too big an ask. Thus, despite more cost-effective proposals such has Rocket Lab’s (still complex) three-launch mission slated to cost a “mere” US $4 billion, the entire idea of a sample return mission has been cancelled as a result of NASA’s budget being tightened.

Space Sunday: hotel on the Moon by 2032? Probably not

A rendering of the GRU Space “version 2” hotel. A possibility, a pipedream or something else? Credit: GRU Space

The commercial space sector is in its infancy, and it is very easy to get caught up in the hype and promises that start-ups in the sector bring with them. At times, this is made worse by publications and media outlets swallowing every statement made by the CEO of SpaceX hook, line and sinker, without applying a modicum if critical thinking (yes, I’m looking at you, Ars  Technica, Space.com, Everyday Astronaut and Marcus House), encouraging publications to act more like PR mouthpieces than offering professional reportage.

Take, for example, Galactic Resource Utilisation (GRU) Space, and their claim that in by 2032, they will be operating the world’s first hotel on the Moon and will follow it up with a larger version before offering the same on Mars; framing the moves as the first necessary steps towards humanity becoming a galactic civilisation.

Exactly how serious this company – comprising two founders and a “consultant” – might be in its aims is unclear. But from the company name (GRU – to close to Felonius Gru, the man who planned to steal the Moon in 2010’s Despicable Me to be coincidence , and likely intended as a “har, har” joke) through to some of their wider claims, it’s hard to see this as little more than (at best) naïve thinking.

Certainly, the company’s website and “whitepaper” give rise to a wealth of questions, in terms of the reality of the idea of a hotel on the Moon, through the claims GRU Space make concerning it, to the claims made by the company’s founder. Given this, it’s hard to know where to start in analysing GRU Space and their entire “plan”; both the website and “whitepaper” are fill with gross over-simplifications and logical fallacies whilst at the same time simply skipping over key aspects and costs required of such an undertaking. Take for, example, the company’s 6-point “master plan”, the first 3 steps of which read:

1.       Build a hotel on the Moon. GRU solves off-world habitation.
2.       Build America’s first Moon base (road, mass drivers, warehouses, physical infrastructure on the Moon).
3.       Repeat on Mars.

Who’d have though establishing facilities on the Moon and Mars would be so “simple”. and that’s ignoring the arse-about face progression of steps 1 and 2 – build your hotel then build the infrastructure to support it? Is that not akin to building a housing estate and then providing the necessary road, power, water, sewage, etc., infrastructure?). I’m also going to ignore step 3 entirely, as it involves everything else I’ll cover in this article – with each one being of far greater magnitude.

Steps 4 through 6 of the “plan” are hardly better, drawing as they do on terms such as the Overton Window, and Kardashev Scale and mixing them with further logical fallacies in order to make a (very poor) case for investment whilst offering objectively misguided / misunderstood parallels together with dichotomies of thinking which further underscore the inherent naivety throughout the “whitepaper”.

GRU Space claims the first step in their endeavour will be a test module. Credit GRU Space

In terms of misguided parallels, the “whitepaper” draws on space tourism and tourism on Mount Everest as demonstrations of the potential for a hotel on the Moon to have mass appeal. In terms of the former, the company points to the rise of space tourism in the last 5 years, presenting a graph suggesting tourism far outweighs astronaut flight into space. However, the data presented ignores the fact that almost 50% of said tourists have participated in sub-orbital flights to the edge of space; a very different proposition to flying to orbit – or the Moon to the point where it has absolutely no bearing on the latter.

Turning to Mount Everest, while it is true that tourism has made up the lion’s share of ascent to the summit of Mount Everest, since the 1990s, less than 8,000 individuals have made the trip to summit of the mountain. Both sub-orbital flights to the edge of space and to the summit of Mount Everest aren’t cheap: the latter comes in at between US $50,000 and US $120,000 for a trip with “good” to “excellent” logistical support; whilst sub-orbital flights cost somewhere in the range of US $225,000-US $400,000. None of these price points are exactly accessible to a mass market. And they don’t come anyway close to the costs GRU Space is projecting. costs presented no sound financial foundation other than vague predications from the likes of the SpaceX CEO (and we all know how accurate those tend to be) .

By their own guessimates, GRU Space are planning to offer 5-night stays at their “Moon hotel” for an initial US $$27,083,335.00 per person, which they claim will fall to just under US $1 million. However you cut it, the first is several orders of magnitude greater than the cost of an 8-minute flight to the edge of space, and enough to make even the very wealthy baulk. The second, meanwhile operates on a false assumption, something I’ll come to in a moment. As such, it is hard to see GRU Space leverage the kind of real money they will need to make their plans a reality.

The GRU Space “version 1” hotel supposedly for 4 guests, an inflatable structure surrounded by shaped regolith. Credit: GRU Space

In terms of cost to customers, the “whitepaper” glosses over / ignores a lot. First, the suggestion they will be using either the Starship HLS or Blue Origin Blue Moon Mark 2 lunar landers – both of which, it is not unfair to say, will have other priorities (assuming the SpaceX HLS actually reaches a point where it can enter service), making their use in a parallel commercial venture somewhat questionable. More to the point: these vehicles will require periodic refuelling to remain operational – at an unknown cost the “whitepaper” fails to mention. More than that, both vehicles require refuelling in order to reach the Moon; no mention of this fact in made in the GRU Space document or who will pay for it.

Given that SpaceX estimate on-orbit refuelling of a Moon-bound Starship will be on the order of US $180 million – that’s a big chunk of missing data – US $45 million per seat in the case of tourists heading for the “version 1” hotel (designed to house  guests), if the cost is to be passed on, which is not mentioned either; neither is how the cost per flight be met if GRU Space is to somehow “absorb” it. There are also other issues around the use of Starship (e.g. whether or not the HLS version will ever be used for anything beyond two Artemis missions and then junked; whether the “standard” version of Starship will ever be rated to launch humans – eve the HLS version will not be rated for crew launches from Earth and so on). however, I’ll do you a favour a pass on waffling on about them.

Of course, Starship is not the only player in town. There’s Blue Origin, a company far more likely at this point in time to deliver humans to the surface of the Moon than SpaceX. But even they require on-orbit and lunar refuelling options, again increasing the overall cost per guest at a GRU Space hotel.

Similarly, the idea that there will be some kind of “10 fold” decrease” in the cost of launching humans into space, making flights to the 12-person “version 2” of the hotel so much cheaper, actually stand up to scrutiny. Whilst Starship has the potential to reduce the cost of launching inanimate payloads to orbit, this is only if it can operate at scale – multiple launches per day. Frankly, the commercial market as a whole is a long way from requiring that kind of general launch cadence, making the idea questionable.

More to the point, whilst SpaceX has reduced the cost per kilo of launching payloads to orbit on Falcon 9, the cost to do the same with humans – $225 million per 4-person launch – has not shifted downwards at all since 2019, despite the 5-fold increase in the Crew Dragon fleet.. This is because launching humans requires a lot of specialised ground and vehicle systems; thus SpaceX look to reductions in servicing and turning around Falcon 9 booster as a means to offset the overheads involved in servicing and refurbishing individual Crew Dragon craft, not as a means to reduce costs to users. There is absolutely no reason to suspect this would not also be the case with and future human rated version of Starship, were it to appear.

Nor does the failure to accurately present costs end there. no mention is made as to:

  • The cost of what would likely be single-use spacesuits for the hotel guests (which could be anywhere from US $10 million to US $228 million, depending on the suit type and manufacturer).
  • The cost of developing and deploying suitable life support systems and their back-up for each hotel; the implementation of suitable power generation and storage capabilities and the parallel need for thermal regulation systems.
  • The costs involved in ensuring adequate on-sit medical facilities.
  • The cost (or number) of staff for each version of the hotel (or in providing them with accommodation, life support, food, etc.).

Perhaps the most glaring example of the naivety present in the “whitepaper” is the claim that GRU Space can recoup all of the outlay involved in establishing the 4-person hotel  – liable to realistically be in excess of at least US $1 billion – by flying just 12 guests to the hotel in the first year.

The only way this potentially comes into the vicinity of being a realistic figure is if the costs of all the essentials mentioned above – power, life support, etc – are ignored, and you look at the claim sideways and in a mirror. With one eye closed and the other squinting, whilst simultaneously reciting Hamlet’s soliloquy in full.

Another rendering of GRU’s “version 2” hotel. Credit: GRU Space

In terms of logical fallacies with the “whitepaper”, these are literally manifold-  places an many as 5 in single statements. I’m not going to list all of them here. But to provide a further example: the whitepaper infers that because NASA requires in-situ resource utilisation (ISRU) for the Artemis Moon base, GRU Space is the only logical choice for providing those capabilities because they are “unique”. In reality, there are multiple companies and universities involved in ISRU technology development, all of whom are far better established than a two-man start-up.

There is much more within the “whitepaper” that can, and should be challenged – and which should have been challenged by space media outlets rather than them simply regurgitating the PR without thought or research but no. Like the equally questionable Voyager Station proposal claiming a company will have a spinning space station (to give it artificial gravity) accepting up to 280 guests (at $1.2 million a pop) operating from 2027 – the PR is presented as reportage that has a Field of Dreams inevitability, with not a single question about where the “tens of billions” required to build the station will come from (indeed, as of writing, Above Space has raised exactly … US $4.8 million over 4 years, and much of the dedicated space media which helped hype the idea seem to have quietly brushed it to one side.

As such, I admit to a certain curiosity as to where GRU Space will be in the hype cycle a year from now. As it is, it would appear that two companies originally cited as “backers” for the project have requested their names be removed from the company’s website: Anduril Space and … SpaceX.  If nothing else, having a company run by the king of over-promising and under-delivering ask for its name to be removed from your  website can’t really be a good sign.

Artemis 2 Update

The Artemis 2 Orion vehicle within its payload fairings and Launch Abort System at the top of the Space Launch System rocket on LC-39B, Kennedy Space Centre during the wet dress rehearsal. Credit: NASA

As per my previous Space Sunday article, Sunday, February 8th, 2026 was targeted as the launch date for the launch of the crewed Artemis 2 mission around the Moon and back.

At that time of that article, NASA was running the mission’s massive Space Launch System rocket through a wet dress rehearsal  (WDR) – a final pre-launch test designed to ensure all ground systems  – including those responsible for loading the vehicle’s core tanks with propellants were all operating correctly and to uncover any niggles in processing, etc. that could be ironed-out before an actual launch.

During the preparations for Artemis 1 in 2022, a similar WDR caused NASA much embarrassment and rolling of the mission’s launch vehicle back and forth between the launch pad and the Vehicle Assembly Building at Kennedy Space Centre (exacerbated by bad weather) due to a series of issues relating to the feeds providing propellants and vital gases to the rocket, including the liquid hydrogen propellant feed located on the mobile launch platform at the base of the rocket.

These issues resulted in significant changes and updates to the umbilical system in the years following Artemis 1, and the Artemis 2 WDR was the first opportunity to test them in sequence. These updates name some at NASA take a bullish attitude towards the WDR and the updates made to the launch systems.

However, as propellant loading progressed, sensors within the umbilical propellant feed system reported a helium leak similar to that seen with Artemis 1, possibly as a result of the neighbouring hydrogen umbilical super cooling the seals on the helium feed, causing them to contract and allow helium to escape. The countdown was paused to allow the helium seals to warm up and reset.

This appeared to work, and the countdown reached  T -5:15. at this point the Ground Launch Sequencer – a system designed to monitor all aspects of the vehicle’s preparations ad make sure everything proceeds in the correct sequence – intervened and shut down the test when it registered multiple sensors reporting a sudden and sustained spike in hydrogen leaking from the umbilical system – much as happened with the Artemis 1 WDR.

As a result, the the February launch opportunities were closed out, and operations moved to the early March launch opportunity to allow the problems with the hydrogen feed to be investigated. This means Artemis 2 will not launch until March 7th, earliest, and will likely be preceded by a further WDR. The leaks and delay are liable to cause further negative feedback towards SLS / Orion – and cause NASA a certain degree of embarrassment.

Artemis 2 on the pad at Kennedy Space Centre. Credit: Craig Bailey. Florida Today

In the meantime, the delay clears Crew 12 for a February 11th launch to the ISS.

Space Sunday: space debris and atmospheric damage + some updates

A European Space Agency Automated Transfer Vehicle (ATV) burns-up in the upper atmosphere following its departure from the International Space Station (ISS). Debris from this type of re-entry burn-up is now of growing concern due it its potential impact on the atmosphere and climate change. Credit: ESA

I’ve written about the issues of space debris on numerous occasions in these pages (for example, see: Space Sunday: debris and the Kessler syndrome; more Artemis or Space Sunday: Debris, Artemis delays, SpaceX Plans). Most of these pieces have highlighted the growing crowded nature of space immediately beyond our planet’s main atmosphere, the increasing risk of vehicle-to-vehicle collisions and the potential for a Kessler syndrome event.

However, there is another aspect of the increasing frequency of space launches and the number of satellites and debris re-entering the atmosphere: pollution and an increase in global warming. This is something I covered in brief back in October 2024, and it is becoming a matter of growing concern.

Currently, there are 14,300 active satellites orbiting Earth (January 2026), compared to just 871 20 years ago. Some 64.3% of these satellites belong to one company: SpaceX, in the form of Starlink satellites. Launches of these commenced in 2019, with each satellite intended to operate between 5 and 7 years. However, because of their relative cheapness, combined with advances in technology and the need for greater capabilities means than since August 2025, SpaceX has been “divesting” itself of initial  generations of their Starlink satellites within their anticipated lifespan at a rate to match the continued use of newer satellites, freeing up orbital “slots” for the newer satellites.

As a result, SpaceX is now responsible for over 40% of satellite re-entries into the atmosphere, equating to a net of over half a tonne of pollutants – notably much of it aluminium oxide and carbonates – being dumped into the upper atmosphere a day, all of which contributes to the greenhouse effect within the upper atmosphere.

These particulates drift down into the stratosphere where monitoring is showing they are having some disturbing interactions with everything from the ozone layer through to weather patterns.

We’re really changing the composition of the stratosphere into a state that we’ve never seen before, much of it negative. We really don’t understand many of the impacts that can result from this. The rush to space risks disrupting the global climate system and further depleting the ozone layer, which shields all living things from DNA-destroying ultraviolet radiation.

– John Dykema, applied physicist at the School of Engineering and Applied Sciences, Harvard

A 2023 axonometric view of Earth showing the space debris situation in different kinds of orbits around Earth. Credit: Pablo Carlos Budassi

In a degree of fairness to SpaceX – who will continue to dominate the issue of re-entry pollutants if their request to deploy a further 15,000 Starlink units is approved – they are not the only contributor. One Web, Amazon, Blue Origin and China via their Qianfan constellation, all stand to add to the problem – if on something of a smaller scale (Amazon and Blue Origin, for example, only plan to operate a total of 8,400 satellites, total). Further, NASA itself is a contributor: the solid rocket boosters used by the space shuttle and now the Space Launch System have been and are major depositors of aluminium and aluminium oxides in the upper atmosphere.

Nor does it end there. The vehicles used to launch these satellites are a contributing factor, whether semi-reusable or expendable. They add exhaust gases – often heavy in carbonates – into the atmosphere, as well as continuing to the dispersion of pollutants in the upper reaches of the atmosphere as upper stages re-enter and burn up.

Carbonates and things like aluminium oxides are of particular concern because of their known impact on both greenhouse gas trapping and in the destruction of the ozone layer. A further factor here is that research suggests that interactions between aluminium oxide and solar radiation in the upper atmosphere can result in the production of chlorine in a highly reactive form, potentially further increasing ozone loss in the atmosphere.

We’re not only putting thermal energy into the Earth’s climate system, but we’re putting it in new places. We don’t really understand the implications of changing stratospheric circulation. It could cause storm tracks to move. Maybe it could shift climate zones, or possibly be a new source of droughts and floods. Chlorine is one of the key actors in the ozone hole. If you add a new surface that converts existing chlorine into reactive and free radical forms, that will also promote ozone loss. Not yet enough to create a new ozone hole, but it can slow the recovery that began after the 1987 Montreal Protocol phased out chlorofluorocarbons.

– John Dykema, applied physicist at the School of Engineering and Applied Sciences, Harvard

There is something of a complex balance in all of this. We need the capabilities an orbital infrastructure can provide – communications, monitoring, Earth and weather observation, etc.,  – but we also need to be aware of the potential for debilitating the natural protections we need from our atmosphere together with the potential for pollutants to further accelerate human-driven climate change beyond the ability of the planet to correct.

This is further complicated by the inevitable friction between commercial / corporate need  – and much of modern space development is squarely in the corporate domain, where income and revenue are the dominant forces – and governmental oversight / policy making and enforcement. As such, how and when policy makers might act is also subject to some complexity, although many in the scientific community are becoming increasingly of the opinion that action is required sooner rather than later, and preferably on a united front.

Changes to stratospheric circulation may ultimately prove more consequential than the additional ozone loss, because the outcomes are so uncertain and potentially far-reaching. For the moment, many questions are not really amenable to straightforward, linear analysis. The ozone loss is significant, and we’re putting so much stuff up there that it could grow in ways that are not proportional to what has thus far been seen. The question is whether policymakers will act on those concerns before the invisible wake of our spacefaring ambitions becomes impossible to ignore.

– John Dykema, applied physicist at the School of Engineering and Applied Sciences, Harvard

Brief Updates

Artemis 2 Launch targets February 8th As Earliest Opportunity

NASA has announced a new earliest launch target date for Artemis 2: Sunday, February 8th, 2026, some two days later than the initial earliest launch date target.

The decision to push the target date back was taken after the planned wet dress rehearsal (WDR) for the launch – which sees all aspects of a vehicle launch tested right up to the point of engine ignition – was postponed due to extremely cold weather moving in over the Kennedy Space Centre which could have impacted accurate data gathering on the 49-hour test, which had been slated to commence on January 29th, 2026.

The Artemis 2 Space Launch System rocket on the pad at Launch Complex 39B at Kennedy Space Centre, January 31st, 2026. Credit: NASA/Joel Kowsky.

The WDR was instead reset for the period of February 1st through 3rd, 2026, with the countdown clock to the start of testing resuming at 01:13 UTC on February 1st. It will run through to the opening of a simulated launch window for 02:00 UTC on February 2nd. This latter part of the test will see the propellant loading system – which exhibited issues during preparations for the 2022 Artemis 1 launch – put through its paces to confirm it is ready for an actual launch.

As a thorough testing of all ground  and vehicle systems, and a full rehearsal for all teams involved in a launch, the WDR is the last major step in clearing the SLS and Artemis 2 for it mission around the Moon. It will officially terminate as the simulated launch window opens, some 10 seconds before engine ignition – but data gathering will continue through until February 3rd as the rocket is de-tanked of propellants and made safe. Then will come a data analysis and test review.

The actual crew of Artemis 2 are not participating in the test, but will be observing / monitoring elements of the WDR as it progresses. NASA has a livestream of the pad as the WDR progresses, and a separate stream will be opened during the propellant loading phases of the test.

The Artemis 2 crew: Canadian Space Agency astronaut Jeremy Hansen, and NASA astronauts Victor Glover (vehicle pilot), Reid Wiseman (mission Commander) and Christine Koch. Credit: NASA

The push back to February 8th, means that NASA effectively has a 3-day opportunity through until February 11th (inclusive) in which to launch the mission before the current window closes. After that, the mission will have to wait for the March launch window to open.

NASA / SpaceX Crew 12 Looks to February 11th Launch

As NASA primarily focuses on Artemis 2, a second crewed launch is being lined up on the taxiway (so to speak) ready to follow the SLS into space – or possibly launch ahead of it.

NASA and SpaceX have confirmed they are looking at February 11th, 2026 as a potential launch date for the Crew 12 mission to the International Space Station (ISS). The mission will lift-off from Kennedy Space Centre’s launch Complex 39A (LC-39A), just a few kilometres away from the SLS at LC-39B, carrying NASA astronauts  Jessica Meir and Jack Hathaway, together with ESA astronaut Sophie Adenot, and Roscosmos cosmonaut Andrey Fedyaev aboard the SpaceX Crew Dragon Freedom.

The Expedition 74/75 / SpaceX Crew 12 personnel, l to r: Roscosmos cosmonaut Andrei Fedyaev, NASA astronauts Jack Hathaway (vehicle pilot) and Jessica Meir (crew commander), and ESA astronaut Sophie Adenot. Image credit: SpaceX.

Officially classified as NASA Crew Expedition 74/75, the four will bring the ISS back up to it nominal crew numbers following the medical evacuation which saw the Crew 11 astronauts make an early return to Earth, as I’ve covered in recent Space Sunday articles.

The preparations for Crew 12’s launch means that in the coming days there will be two rockets on the pads at Kennedy’s Launch Complex 39, each proceeding along its own route to launch. As to which goes first, this depends primarily on how the Artemis 2 / SLS launch preparations go.  If it leaves the pad between February 8th and February 10th as planned, then there is nothing hindering Crew 12 lifting-off atop their Falcon 9 booster. However, any push-back to February 11th would likely see Crew 12 delayed until February 12th at the earliest. Conversely, if Artemis 2 is delayed until the March launch opportunity, this immediately clears the way for Crew 12 to proceed towards a February 11th lift-off, with both February 12th and 13th also available.

Habitability of Europa Takes Another Blow

In my previous Space Sunday article, I covered recent studies relating to the potential for Jupiter’s icy moon Europa to harbour life (see: Space Sunday: examining Europa and “The Eye of Sauron”). The studies in question were mixed: one contending that conditions on Europa might lean towards life being present within its deep water ocean, the other being more sceptical about the sea floor conditions required to support life (e.g. the presence of hydrothermal vents).

Now a further study has been published, and it also suggests the chances of life existing in Europa’s ocean are at best thin.

One of the core issues with Europa has been knowing just how thick its ice shell actually is. Some have suggested it could be as little as 2 kilometres thick, whilst others have stated it could be as deep as 30km.

Understanding the thickness of the moon’s ice crust is crucial, as it helps define whether or not processes seen to be at work on the Moon are sufficient enough to have an impact on what might be happening within any liquid water oceans under the ice.

If the ice crust is thin – say a handful of kilometres or less – then activities like subduction within the ice sheets have a good chance of carrying minerals and nutrients created by the interaction between brines in Europa’s surface ice down into the ocean below, where they might help support life processes. similarly, transport mechanisms within the ice could carry oxygen generated as a result of surface interactions down through the ice and into the waters below. If the ice is too thick, then there is a good chance such processes grind to a halt long before they break through the ice crust into the waters below, thus starving them of nutrients, chemicals and gases.

An analysis of data gathered by NASA’s Juno mission as it loops its way around Jupiter and making periodic fly-bys of Europa now suggests that the primary ice crust of Europa is potentially some 28-29 kilometres thick. That’s not good news for the moon’s potential habitability because, as noted it would severely hamper any movement of minerals and nutrients down through the moon’s ice and into the waters below. However, the researchers do note that this doesn’t mean such elements could not reach the waters below, but rather they would take a lot longer to do so, but rather their ability to support any life processes within Europa’s waters would be greatly diminished.

A study of data gathered by NASA’s Juno mission spacecraft suggests the thickness of Europa’s ice crust might be enough – 28-20 km – to severely limit the ability of transport mechanisms and “crustal delamination” (see: Space Sunday: examining Europa and “The Eye of Sauron”) to transfer nutrients, chemicals, gases and minerals formed on the moon’s surface down to the liquid water ocean where they might help life processes in the water. Image credit: NASA

An unknown complication here is he state of the ice towards the bottom of the crust. Is it solid all the way through, or does it become more slush-like as it nears the water boundary layer, warmed by the heat of Europa’s mantle as it radiates outward through the ocean? If it is more slush-like, even if only for around 5 kilometres, this might aid transport mechanisms carrying nutrients, minerals, chemicals and oxygen down into the ocean. Conversely, if the ice is solid and there is a further 3-5 km thick layer of icy slush forming the boundary between it and liquid water, then it will act as a further impediment to these transport mechanisms being able to transfer material to the liquid water ocean.

As a result of this study, and the two noted in my previous Space Sunday article, eyes are now definitely turning towards NASA’s Europa Clipper, due to arrive in orbit around Jupiter in 2030, and ESA’s Juice mission, due to arrive in 2031, in the hope that they will be able to provide more detailed answers to conditions on and under Europa’s ice.

Space Sunday: examining Europa and “The Eye of Sauron”

A true colour image of Europa, captured by NASA’s Juno spacecraft during its 45th passage around Jupiter (Perijove 45), October 2023. Credit: NASA/JPL

One of the most fascinating places in the entire solar system is Europa, the second innermost of the four Galilean moons of Jupiter, and the smallest – although “smallest” here being a relative term, Europa (diameter around 3,100 km) being only very slightly smaller in size than our own Moon (diameter approx 3,475 km).

As I’ve explained in past Space Sunday pieces, Europa is subject to similar gravitational flexing as seen on Io, the innermost of the four Galilean moons. This flexing, caused by the unequal push-pull of Jupiter’s immense gravity on one side and the unequal yet effectively combined gravitational pull of the other three Galilean moons on the other, has marked Io as the most volcanically active body in the solar system with upwards of 400 active volcanoes marking its surface.

A rendering of Europa’s interior, as the modern consensus of opinion see it: a thin (10-30 km) outer crust with a water ocean approx 100 km deep, either fully liquid or a mix of liquid water and semi-frozen ice and slush, and a large rocky mantle heated by an iron core due to gravitational flexing. Credit: Kelvinsong

In Europa’s case, the common consensus has been that this flexing is sufficient to cause its core to stretch and contract, generating heat which keeps the waters trapped under the icy crust in a largely liquid state. It has also been hypothesised that this flexing could give rise to ocean floor hydrothermal vents and fumaroles, spewing heat, chemicals and minerals into the ocean; elements which might have kick-started life within Europa’s waters, much as we have seen around similar deep ocean hydrothermal vents here on Earth.

However, there are two stumbling blocks with these ideas. The first is whether or not there is sufficient energy being generated deep within Europa needed to drive a tectonic-like motion in the mantle and cause hydrothermal venting. The second is that, even with the minerals and chemicals blasted out of deep ocean fumaroles here on Earth, our oceans are rich in nutrients vital for life generated by things like the constant death and decay of marine life, the interaction of solar radiation with salts and other minerals within the upper reaches of our oceans, etc., and which are carried down to the depths by the natural cycles present within our oceans and help drive the life processes fund around deep water fumaroles.

A rendering showing the tidal heating processes believed to be at work in Europa, allowing it to have a liquid water ocean and – possibly – hydrothermal vents. Credit: NASA/JPL

While it is known that Europa has interactions between the intense radiations given off by Jupiter and the salts and minerals in its surface ice (giving rise to the discolouration seen across much of the moon) which likely give rise to chemicals and nutrients, how these might get down through the ice into the ocean below remains a unclear – although one theory suggests subduction might be a suitable mechanism.

A recently published study by geophysicists at Washington State University and Virginia Tech offers a more novel idea: crustal delamination. This is a geological process long known on Earth whereby our planet’s tectonic movement gradually “squeezes” a zone of the planet’s crust, chemically densifying it until it detaches from the crust and sinks into the mantle.

Diagram illustrating the theorised model of a possible avenue toward a form of crustal delamination in a planetary ice shell like Europa’s. Credit: The Planetary Science Journal (2026). DOI: 10.3847/PSJ/ae2b6f

Europa’s icy crust is in a degree of motion thanks to the aforementioned flexing. As noted above, this gives rise to the potential of subduction pushing “plates” of ice under others. Whether or not this is strong enough to push nutrient-laden ice down to the level of the ocean is unclear. However WSU / Virginia Tech study suggests the flexing, breaking and reforming of Europa’s surface ice could result in a unique kind of “crustal delamination”, with their model suggesting it could allow pockets of mineral and nutrient rich ice to “burrow” down to the warm liquid ocean, melt and release their nutrients into Europa’s supposed thermal currents.

If correct,  this could allow Europa to provide the kind of nutrients any life down on its ocean floor. What’s more, it’s a theory that works within the subduction model, allowing the two to work together in the supply of nutrients and chemicals into Europa’s waters.

The “crustal delamination” theory sits will with other theories for ice movement on Europa, such as subduction. Credit: NASA

All of which bodes well for the theory that Europa may be an abode for life. However, another study authored by a team of leading planetary science experts concludes that suggests that whilst the competing gravitational forces at work on Europa might be sufficient to cause the moon to flex, but are insufficient to cause any kind of hydrothermal venting on the moon’s ocean floor.

If we could explore that ocean with a remote-control submarine, we predict we wouldn’t see any new fractures, active volcanoes, or plumes of hot water on the seafloor. Geologically, there’s not a lot happening down there. Everything would be quiet.

– Paul Byrne, an associate professor of Earth, environmental, and planetary sciences

This conclusion was reached after taking data on Europa’s size, the likely make-up of its deep core and surrounding mantle, its orbit, and on the likely gravitational forces at work on the moon. In particular, the study also contrasted the orbit of Io with that of Europa, and the role it plays in Io’s extreme volcanism.

Io occupies something of an erratic orbit and this increases the amount of influence gravities of Jupiter and the other three Galilean Moons have on it. But Europa’s orbit is closer to circular, and less prone to gravitational extremes, thus reducing the overall amount of flexing the moon experiences, greatly reducing the likelihood of any internal heating driving the kind of “tectonic”-like shifts in Europa’s mantle needed for venting to occur.

Europa likely has some tidal heating, which is why it’s not completely frozen. And it may have had a lot more heating in the distant past. But we don’t see any volcanoes shooting out of the ice today like we see on Io, and our calculations suggest that the tides aren’t strong enough to drive any sort of significant geologic activity at the seafloor.

– Paul Byrne, an associate professor of Earth, environmental, and planetary sciences

The key point here is that whilst a form of crustal delamination may well be at work alongside subduction to deliver vital nutrients for life deep into the waters of Europa’s oceans, without the hydrothermal venting acting as a direct energy and chemical / mineral source required to give that life a kick-start, the chances are, those nutrients aren’t really helping anything.

All of which make the discoveries NASA’s Europa Clipper and ESA’s Juice mission might make when they reach the Jovian system in the 2030s and start probing Europa’s secrets in great detail, all the more intriguing.

Blue Origin Confirm NG-3 Mission; Rocket Lab Suffer Neutron Setback

Two missions provisionally set for launch in the first quarter of 2026 received updates both good and bad (and a little curious in the case of one) this week.

The good / curious update came from Blue Origin with the confirmation of the next flight of their New Glenn heavy lift launch vehicle (HLLV). In it, the company indicated they are on course to launch New Glenn on its third flight towards the end of February 2026, and that it will utilise the core booster stage called Never Tell Me The Odds, used in the second flight of New Glenn – NG-2 – which set NASA’s twin ESCApades satellites on their way to Mars. Thus, the mission will be the first to see the re-use of a New Glenn core stage.

Never Tell Me The Odds, the New Glenn core stage used for the NG-2 launch in November 2025, sitting on the landing vessel Jacklyn following its flight in that mission. It is now set to be re-used in the NG-3 launch, currently targeted for late February 2026. Credit: Blue Origin

The curious element of the announcement lay in the payload for the mission – NG-3. Following NG-2, Blue Origin had indicated they would be looking to launch their Blue Moon Pathfinder mission to the Moon on NG-3, also reusing Never Tell Me The Odds in the process. However, this mission has now been moved back in the company’s launch manifest and, at the time of writing, has no indicated launch period other than “2026”. Instead, NG-3 will launch a 6.1 tonne Bluebird communications satellite to low Earth orbit (LEO) on behalf of AST SpaceMobile, helping to expand that company’s cellular broadband constellation.

Blue Origin has not stated any reason for the payload swap or whether it is due to requiring more time to prepare the Blue Moon demonstrator lander or not. It might be that the company needs more time in preparing Blue Moon, or it might be because they’d rather launch that mission using a new core booster; or it might be because they want to gather more data on vehicle performance carrying heavier payloads. The first two launches carried around 2-3 tonnes and just over a ton respectively. Blue Moon masses almost 22 tonnes, a sizeable jump, whereas Bluebird is a more modest increment.

Meanwhile, Rocket Labs suffered a setback which spells the end of their hopes to debut their Neutron rocket in the first quarter of 2026 – and which might delay the vehicle’s maiden flight by as much as a year.

Neutron is intended to be a 2-stage, partially-reusable medium lift launch vehicle (MLLV) in roughly the same class as ULA’s Vulcan-Centaur and SpaceX’s Falcon 9. However, it is of a highly innovative design, the second stage of the vehicle and its payload being carried aloft inside the first stage, within a set of clamshell payload fairings the company calls the “hungry hippo”. These open once the rocket has cleared the Earth’s denser atmosphere so the payload and its motor stage can be released, the core stage then returning to land on a floating platform.

A video showing the 2025 ground testing of Neutron’s aerodynamic fins, which will be used in the core stage’s descent to a landing barge touchdown, and the “Hungry Hippo” payload fairing forming the nose of the stage 

The first Neutron vehicle (sans its upper stage and payload) arrived on the pad at rocket Lab’s launch facilities at the Mid-Atlantic Region Spaceport (MARS) on the Virginia coast earlier in January. On January 21st, the vehicle was undergoing a hydrostatic pressure trial intended to validate structural integrity and safety margins so as to ensure a successful launch.  However, during the test, the vehicle’s main propellant tank buckled and then ruptured, effectively writing off the rocket.

Rocket Lab will now need time to analyse precisely what went wrong, why the propellant tank gave way and whether any significant structural alterations need to be made to it prior to any launch attempt being made.

A rendering of Rocket Lab’s Neutron and how it will work. Credit: Tony Bella

Gazing into the “Eye of Sauron”

Our Sun will one day die. In doing so, its hydrogen depleted, it will swell in size as it struggles to consume progressively heavier elements within itself before it collapses once more, shedding its outer layers into what we call a planetary nebula. It’s not a unique end for a main sequence star such as the Sun, but it can be a beautiful one when viewed from afar and through the eyeglass of time.

One such planetary nebula is that of NGC 7293 / Caldwell 63, commonly referred to as the Helix Nebula. Located some 650 light years away within the constellation of Aquarius as seen from Earth, it is one of the closest bright planetary nebulae to our solar system.

A nine-orbit, true colour image of the Helix Nebula captured by the Hubble Space Telescope (HST) revealing the structure of of nebula. Credit: NASA / ESA / STScl

Formed by an intermediate mass star thought to be similar to the Sun, the Nebula takes its name by the fact that the outer layers  look – from our perspective, at least – like a helix. Some 2.9 light years across its widest axis, the nebula features the stellar core of the star which created it near its centre, a core so energetic as it collapses towards becoming a white dwarf it blew off, it causes the layers of gas and dust to brightly fluoresce.

This combination of shape and fluorescing colours has given the nebula two additional informal names:  The Eye of God, and more latterly and partially in fun in the wake of the Lord of the Rings films, The Eye of Sauron. The nebula was perhaps first made famous by a nine-orbit campaign using the Hubble Space Telescope to capture true-colour images of it in 2004, resulting in a stunning (at the time) composite image of the nebula.

In 2007, the Spitzer Space Telescope captured the Helix Nebula in the infrared wavelengths, revealing much of the complex structure of the nebula’s gas and dust layering, with the core remnants of the star forming it clearly visible and blood red taking to the infrared, giving it the appearance of an eye.

An nfrared false-colour image of the Helix Nebula from the Spitzer Space Telescope. The white dwarf at the heart of the nebula appears red in this image, suggesting a malevolent eye. Image Credit: NASA/JPL

More recently, both the European Southern Observatory’s (ESO) VISTA (Visible and Infrared Survey Telescope for Astronomy) wide-angle telescope located high in the Atacama Desert of Chile, and NASA’s James Webb Space Telescope (JWST) 1.5 million km out in space, have caught the full majesty of the Helix Nebula in comparative detail.

In particular, the JWST images reveal much of the intricate nature of the layers of gas and dust within the nebula. These include clear signs of how the powerful pulses of stellar wind from the dying star are forcing most of the gases and dust in the layers to be pushed away from the core, with globular-like knots and strands of denser material resisting the push, forming what is called cometary knots, due to their resemblance to comets and their tails. However, these “comets” tend to be wider than the planetary core of our solar system!

Left: a true-colour, high-resolution of the Helix Nebula captured by ESO’s VISTA The image of the Helix Nebula on the left is from the ESO’s VISTA telescope in Chile. Right: an image from JWST offering detail on a portion of the Nebula. Credits: ESO/VISTA / NASA / ESA / STScI, J. Emerson (ESO)

JWST’s images also reveal the blue heat of stars beyond the nebula diffracted into beautiful star-like forms by the intervening (and invisible) gas and dust. VISTA, meanwhile helps put the JWST images into perspective within the Nebula as a whole. They also demonstrate how it was likely Helix was result of three different outbursts – or epochs – from the star.

The innermost of these epochs is obviously the youngest and more intact and more exposed to the outflow of stellar winds from the star’s remnants, whilst the outermost is interacting with the interstellar medium, with evidence of shockwaves, ripples, and a general “flattening” of the expanding clouds as it collides with the increasingly denser gas within the interstellar medium. This outermost layer was likely formed about 15,000-20,000 years ago, with the innermost about 10,000-12,000 years old.

A close-up image from JWST showing the “cometary knots”, the majority likely larger than the planetary core of our solar system, formed by dense clusters of gas resisting the outward push of solar winds from the dying star. A star is shown in blue, indicating its heat, the light from it undergoing diffraction by the non-visible dust and gas of the nebula. Credit: NASA / ESA / STScl

In time – around 30-50,000 years from now – the Helix Nebula will vanish as it merges into the interstellar medium and its star collapses into a quiescent white dwarf. But for now it continues to turn its eye upon us, gazing down as an entrancing ring of beauty, visible to professional and amateur astronomers alike.