Space Sunday: space stations, Vulcans, rockets

A Northrop Grumman Cygnus resupply vehicle approaches the International Space Station (ISS) to deliver supplies. Credit: NASA

ISS Updates

In a further sign that the International Space Station is in its final decade of operations, NASA is seeking to extend the current contracts for re-supply missions to the station from the period January 2027 through December 2030, in what is referred to as a “final” contract period.

In March 2022, NASA awarded additional contracts for ISS re-supply missions through until the end of 2026 to SpaceX (Cargo Dragon) Northrop Grumman (Cygnus) and Sierra Space (Dream Chaser Cargo). Under the extension, all three companies will be allowed to bid on remaining re-supply mission slots through until December 2030, but contract opportunities will not be issued to additional companies beyond these three.

Under the current contract, SpaceX are required to fly a total of 15 resupply missions through until the end of 2026, at an average of US $157 million per flight; Northrop Grumman 14 Cygnus flights at an average of US $150 million; and Sierra Space three Dream Chaser Cargo flights at US $367 apiece. It is not clear if any additional flights granted between January 2027 and December 2030 will be at the current rates or whether the three companies will seek to raise their fees – with the 2018 contract extension, SpaceX hiked their fees by 50%.

SNC’s uncrewed Dream Chaser Cargo and its external cargo module, which will also supply electrical power to the vehicle. Credit: Sierra Space.

No further re-supply missions to ISS to be scheduled beyond 2030, that is the year the station is to be decommissioned and the majority of it de-orbited to burn up in the atmosphere, with any surviving elements crashing into the Pacific Ocean at Point Nemo – the area of that ocean furthest of land in any direction. However, modules due to be delivered to the ISS by Axiom Space starting in 2025 will be detached to form the nucleus of a new private-sector space station.

Currently, it is not clear whether Russia plans to remain with the ISS programme through until 2030 or withdraw some time before. In 2022, the country announced plans to withdraw “after 2024” (which many pundits took to mean “from 2025”) in order to focus on a national space station – the Russian Orbital Service Station. The power module for this new station had originally been slated for 2024, with the core module targeting 2025. However, the power module will now not launch before 2027, and the core module “no earlier” than 2028, so it would seem likely Russia will remain engaged in ISS operations through until at least then.

A model of the Russian Orbital Service Station during the Russian Federation’s International Military-Technical Forum “Army”, August 2022, complete with Soyuz replacement crew vehicle (foreground). Credit: Kirill Borisenko

In the interim, there was a degree of excitement aboard the ISS in the past week. At 12:42 UTC on Monday, March 6th, 2023, the ISS has to use the thrusters on the Progress M-22 re-supply vehicle currently docked at the station’s Zvezda module to avoid a potential collision with an orbiting satellite.

The satellite in question – believed to be Nusat-17, part of an Argentinean earth observation constellation, the majority of which were launched in the 2020s, and all ten satellites in the network are in orbits deteriorating towards that of the ISS. The potential for collision was known in advance, allowing the orbital boost – called a pre-determined avoidance manoeuvre (PDAM) – to be completed with the minimum of fuss, the Progress firing its thrusters for 6 minutes and without disruption to overall ISS operations.

The manoeuvre marked the 33rd such change to the station’s orbital track resulting from the risk of collision since 1999, and there is mounting concern that the greater use of low-altitude constellations of satellites such as those operated by SpaceX Starlink and the UK’s OneWeb could see the ISS facing greater exposure to potential collisions over the next 7-8 years.

A graph showing the numbers of ISS collision avoidance manoeuvres between 1999 and 2023. Credit: NASA Orbital Debris Program Office (ODPO)

The distraction of the manoeuvre was not enough to delay preparations for the return of NASA’s Crew 5 mission from the ISS aboard SpaceX Crew Dragon Endurance, with the vehicle departing the ISS on Saturday, March 11th, 2023 at 0720 UTC. Aboard were NASA astronauts Josh Cassada and Nicole Mann, together the Japanese astronaut Koichi Wakata and cosmonaut Anna Kikina of Russia, returning home after 157 days on-orbit aboard the ISS, and having completed a hand-over to the personnel of Crew 6, who arrived at the ISS on March 3rd.

After undocking, Endurance performed a series of orbital manoeuvres throughout the day, prior to completing re-entry to splashdown off the Florida coast at 02:02 UTC on Sunday, March 12th, bringing to an end a mission marked by firsts: Mann being the first Native American to reach orbit; Kikina the first Russian national to fly on a private US space vehicle, and Wakata setting the record for the longest cumulative time a Japanese astronaut has spent in space thus far – 505 days in total. He is also the only Japanese astronaut to fly into space in three different space craft: the US space shuttle (4 times), Soyuz (once) and Crew Dragon (once).

The Crew 5 team, clockwise from bottom: Koichi Wakata, Anna Kikina, Josh Cassada and Nicole Mann. Credit: NASA

The Russian space agency Roscosmos is turning its eyes to the that the recent coolant leaks which left the crew of Soyuz MS-22 without a ride back to Earth and also affected Progress MS-21 towards a manufacturing fault.

Russian mission managers initially blamed a micrometeoroid strike on the leak which crippled Soyuz MS-22 on December 14th, 2022. However, when the Progress vehicle (referred to as Progress 82 by NASA) suffered a similar, but lesser rupture in its coolant loop, questions started to be asked as to whether something else was to blame – the Soyuz and Progress vehicles are essentially the same vehicles using the same systems, with the exception that Progress had none of the crew facilities or life support systems, instead being equipped for carrying cargo; they are also without any heat shield, so the entire vehicle burns-up on re-entering the atmosphere.

With Progress MS-21, Roscosmos stated the leak, which occurred in February, was the result of a launch incident five months before the vehicle docked with the ISS. However, Roscosmos has now joined with Soyuz / Progress manufacturer Energia to investigate a possible manufacturing issue affecting both vehicles – particularly given the failures occurred after both craft had been in space for roughly the same amount of time, suggesting some form of related failure.

Progress data. Credit: Karl Tate

As I noted in my previous Space Sunday update, Soyuz MS-22 has been replaced at the International Space Station (ISS) by MS-23, which is intended to provide the crew of Frank Rubio (NASA) and cosmonauts Sergey Prokopyev and Dmitry Petelin with a ride home in September 2023. However, NASA in particular is monitoring it and Progress MS-22 (launched in February 2023) for any signs of problems as the vehicles remain at the station.

Continue reading “Space Sunday: space stations, Vulcans, rockets”

Space Sunday: ISS, a lunar time zone and an aurora

Russia’s uncrewed Soyuz MS-23 spacecraft approaches the International Space Station for docking on Feb. 25, 2023. The round forward section of the vehicle is the orbital crew module, discarded before re-entry; the bell-shaped centre element is the Earth return capsule, and the aft end with the solar arrays provides power and propulsion, but is discarded before re-entry. Credit: NASA TV

Russia’s uncrewed Soyuz MS-23 launched for the International space station on February 24th, 2023, on its way to replace the Soyuz MS-22 vehicle struck by a major coolant leak in December 2022, leaving it incapable of returning crew members Sergey Prokopyev, Dmitri Petelin and Frank Rubio to Earth as planned at the end of their 6-month rotation.

Due to the lack of any return capability, NASA and Roscosmos had worked on an emergency scenario whereby the Soyuz seat for Rubio had been transferred to Crew Dragon Endurance to allow his return with the 4-person members of NASA’s Crew 5 in the event of an emergency evacuation being called for ahead of MS-23’s arrival; the theory being that this would reduce the heat load in the Soyuz return capsule, allowing Prokopyev and Petelin to survive a return to Earth in that vehicle.

Having arrived at the ISS on February 25th, the crew started work in off-loading the ~430 kg of cargo MS-23 carried to the ISS and then moving the flight seats for the MS-22 crew into the newly-arrived Soyuz. It is not clear when MS-22 will be undocked from the ISS to attempt an automated return to Earth; however, its crew will now spend almost a year in space, as MS-23 will not make a return to Earth until September 2023, giving Roscosmos time to completely reshuffle crew rotations.

Crew Dragon Endeavour is lifted off of Pad 39-A at Kennedy Space Centre, Florida by a SpaceX Falcon 9 at the start of the Crew 6 mission, March 2nd, 2023. Credit: Jordan Sirokie

In the meantime, NASA’s Crew 6 mission launched from Kennedy Space Centre on March 2nd, aboard SpaceX Crew Dragon Endeavour delivering NASA astronauts Stephen Bowen and Warren Hoburg, cosmonaut Andrey Fedyaev and Emirati astronaut Sultan Alneyadi to the space station on March 3rd, after a one-hour delay in docking whilst a faulty sensor on the docking system was corrected.

Bowen is due to take over the role of ISS commander from Prokopyev, marking the start of NASA Crew Rotation 69. Following handover, the Crew 5 mission, comprising NASA astronauts Nicola Mann and Josh Cassada, together with JAXA astronaut Koichi Wakata and cosmonaut Anna Kikina (the first Russian to fly a US commercial crew programme flight, and the first Russian to fly on a US spacecraft since 2002) will depart the ISS aboard Endurance for Earth, possibly around March 8th.

The NASA Crew 6 / Expedition 69 crew (in the blue jumpsuits) of (l to r) Sultan Alneyadi, Stephen Bowen, Andrey Fedyaev and Warren Hoburg, join the current ISS crew of (l to r foreground) Josh Cassada, Koichi Wakata and Frank Rubio, together with (l to r in the rear), Dmitri Petelin, Sergey Prokopyev, Anna Kikina  and Nicole Mann. Credit: NASA TV 

Crew 6 almost marks the last flight of Crew Dragon under the initial contract between NASA and SpaceX which pegged launch fees at US $220 million / US$55 million per seat.  From the August Crew 7 launch through until Crew 14 (~2028), SpaceX Crew Dragon flights will average US $288 million / US $72 million per seat.

Giving the Moon its Own Time Zone

A human return to the Moon and the potential for establishing a permanent presence there involves many things. Most of the time, efforts are focused on the technologies required: launch and landing systems, communications system, life support, etc. However, one thing people likely do not consider is the matter of how time will be kept.

Until now, missions to the Moon have operated on a time frame based on their country of origin, with their onboard chronometers synchronised with terrestrial time. However, this will not work going forward, when there will be multiple missions – crewed and robotic – operating on and around the Moon.

To facilitate these missions, NASA and the European Space Agency (ESA) are developing new orbital services such as the Lunar Communications Relay and Navigation System and Moonlight, both of which might be thought of a combination of communications as GPS data services such as the US GPS and European Galileo systems.

The latter have their own timing systems, but they possess offsets relative to one another of just a few billionths of a second, allowing them to operate on concert. In particular, they are fixed to the Universal Coordinated Time (UTC) global standard, which is also used by the internet and aviation, as well as scientific experiments that require highly precise time measurements. This allows both networks to remain fully in synch with one another and with ground-based units.

ESA’s Moonlight initiative plans to expand satellite-navigation coverage and communication links to the moon. Credit: ESA / K Oldenburg

Having a universal time standard for the Moon and cislunar space is important because clocks run slower on the Moon’s surface than on Earth by 56 millionths of a second per terrestrial day, whilst clocks placed in different orbits around the Moon will run at different rates to one another and those on the lunar surface. Over time, this can result in communications and data errors to be introduced, so having a singular reference point – time zone – unique to lunar operations is essential for such time-keeping and allowing for things like accurate navigation across the surface of the Moon and when in orbit around it.

To this end, and following meetings hosted by ESTEC, the European Space Research and Technology Centre, space organisations such as NASA, ESA and JAXA, have agreed to develop LunaNet. Based on the core concepts of GPS and Galileo, LunaNet is intended to provide a set of mutually agreed-upon standards, protocols and interface requirements for inter-operability between multiple space and surface units operating around on the Moon, all utilising the same time standard.

Exactly how this standard will be defined and will be responsible for maintaining it or what it should be called has yet to be determined. UTC, for example, is not maintained by any one nation, but by the intergovernmental International Bureau of Weights and Measures (IBWN) based in Paris, France. One suggested name for the new time zone is “selenocentric reference frame” (SRF), which doesn’t exactly roll off the tongue. It has also yet to be decided whether or not it should be synchronised with time zone on Earth. However, as a necessary requirement, developing and defining it could help with future deep-space missions.

UK Treated to Almost Nationwide Auroral Display

On February 24th and again of February 25th, the Sun gave off a pair of coronal mass ejections (CMEs) – massive eruptions of material throwing billions of tonnes of energetic material from the corona and free of the Sun’s gravity well. CMEs are a common event and can move in any direction relative to the Sun. As it so happened, this pair fired Earthward, travelling at around 3 million km/h, each arriving at a time when they were ideal viewing in the evening skies over the UK.

February 26th, 2023 auroral display seen from Hopeman Beach, Scotland. Credit: Alan Tough

After a journey of 150 million km, the material from the first CME slammed into the Earth’s magnetosphere over an UK just settling down for a quiet evening under clear skies on Sunday, February 26th. The result was a sizeable geomagnetic storm in which electrons in the magnetosphere were accelerated into the atmosphere by the blunt force of the CME material, sparking intense auroral displays which rapidly spread far further south than is usually the case, giving people across Britain with a glorious display.

Twenty-four hours later, the second CME struck, this time coinciding with lunchtime in the UK and largely overcast skies. However, such was the nature of the resultant geomagnetic disturbance, coming hard on the heels of the first, resulted in a second extensive auroral display which was still visible  in the evening across many parts of the UK as the skies darkened – and the weather cleared again.

Continue reading “Space Sunday: ISS, a lunar time zone and an aurora”

Space Sunday: asteroid impacts; ISS update

International work on near-Earth asteroid detection systems is again ramping up as, coincidentally, a very small asteroid caused a stir in northern Europe and the UK.

2023 CX1 (originally known as Star2667 prior to its impact) was broadly similar in nature to the type of object such systems would attempt to seek out, in that it was entirely unknown to astronomers the world over until a mere seven hours before it entered Earth’s atmosphere on February 13th, 2023. Fortunately, it was small enough and light enough – estimated to be around 1 metre across its largest dimension and weighing about 1 kilogramme – to pose no direct threat, although its demise was seen from France, the southern UK, Belgium, The Netherlands and northern Spain.

Thus far, over 30,600 asteroids and comets of various classes have been identified as having some risk of striking Earth’s atmosphere, with around 8% know to be of a size (+100m across) large enough to result in significant regional damage should it to so. However, even asteroids and comet fragments of just 20-40m across could cause considerable damage / loss of life were one to explode in the atmosphere over a population centre, whilst the total number of potential threats remains unknown.

A major problem in identifying these objects from Earth’s surface using visual or infra-red means is that the Sun tends to sharply limit where and when we can look for them, whilst radar has to be able to work around 150,000 satellites and all debris and junk we have put in orbit (excluding military satellites and “constellations” of small satellites such as SpaceX Starlink and OneWeb).

To bypass such problems, the European Space Agency plans to deploy NEOMIR, the Near-Earth Object Mission in the Infra-Red, a spacecraft carrying a compact telescope and placed at the L1 Lagrange point between Earth and the Sun (where the gravitational attraction of the two essentially “cancel each other out”, making it easier for a craft occupying the region to maintain its position). From here, Earth and the space around it would be in perpetual sunlight and the Sun would be “behind” the satellite, meaning that any objects in orbit around Earth or passing close to it will also be warmed by the Sun (and so visible in the infra-red), whilst sunlight would not be able to “blind” the satellite’s ability to see them.

An artist’s impression of NEOMIR occupying the Sun-Earth L1 position as it observe the space around Earth for potential near-Earth asteroids which may pose a threat. Credit: ESA

The half-metre telescope carried by NEOMIR will be able to identify asteroids as small as 20m in size, and would generally be able to provide a minimum of 3 weeks notice of a potential impact with Earth’s atmosphere for objects of that size (although under very specific edge-cases the warning could be as little as 3 days), with significantly longer periods of warning for larger objects.

Currently, NEOMIR is in the design review phase, and if all goes well, it will be launched in 2030. In doing so, it will help plug a “gap” in plans to address the threat of NEO collisions with Earth: NASA’s NEO Surveyor mission, planned for launch in 2026, will also operate from the L1 position – but is only designed to spot and track objects in excess of 140m in diameter. Thus, NEOMIR and NEO Surveyor will between them provide more complete coverage.

At the same time as an update on NEOMIR’s development was made, China announced construction of its Earth-based Fuyan (“faceted eye”, but generally referred to as the “China Compound Eye”) radar system for detecting potential asteroid threats is entering a new phase of development.

The first phase of the system – comprising four purpose-built 16m diameter radar dishes – was completed in December 2022 within the Chongqing district of south-west China. Since then, the system has been pinging signals off of the Moon to verify the  system and its key technologies.

Two of the Fuyan 16m radar dishes on test in China, December 2022. Credit: CGTN

The new phase of work will see the construction of 25 radar dishes of 30m diameter, arranged in a grid. When they enter service in 2025, they will work in concert to try to detect asteroids from around 20-30m across at distances of up to 10 million km from Earth, determining their orbit, composition, rotational speed, and calculate possible deflections required to ensure any on a collision course with Earth do not actually strike the atmosphere.

As this second phase of Fuyan is commissioned, a third phase of the network will be constructed to extend detection range out to 150 million km beyond Earth. At the same time, China is planning to run its own asteroid deflection test similar to the NASA Double Asteroid Redirection Test mission, although the precise timeline for this mission is not clear.

An artist’s impression of the Fuyan grid of 25 radar units due to commence operations in 2025. Credit: CGTN

In the meantime, 2023 CX1 was of the common type of near-Earth asteroids to regularly strike Earth’s atmosphere (at the rate of one impact every other week). It was discovered by Hungarian astronomer Krisztián Sárneczky, at Konkoly Observatory’s Piszkéstető Station within the Mátra Mountains, less than 7 hours before impact.

At the time of its discovery it was 233,000 km from Earth (some 60% of the average distance between Earth and the Moon), and travelling at a velocity 9 km per second. It took Sárneczky a further hour to confirm it would collide with Earth, marking 2023 CX1 as only the 7th asteroid determined to be on a collision with Earth prior to its actual impact.

A graphic showing data on dangerous asteroids as of 2020. Credit: ESA Planetary Defence Office

The object – at that time still designated Star2667 – was tracked by multiple centres following Sárneczky’s initial alert, allowing for its potential entry into and passage through the upper atmosphere to be identified as being along the line of the English Channel, close to the coast of Normandy. It was successfully tracked until it entered Earth’s shadow at around 02:50 UTC on February 13th, just 9 minutes before it entered the upper atmosphere

As both the media and public were alerted to the asteroid’s approach, it’s demise was caught on camera from both sides of the English channel. It entered the atmosphere at 14.5 km/s at an inclination 40–50° relative to the vertical. As atmospheric drag increased, it started to burn up at an altitude of 89 km, becoming a visible meteor. At 29 km altitude it started to fragment, completely breaking apart at 28 km altitude as a bright flash as its fragments vaporised, finally vanishing from view at 20 km altitude, although meteorites fell to Earth in a strewn field spanning Dieppe to Doudeville on the French coast, sparking a hunt for fragments to enable characterisation of the object.

At the time of flash-fragmentation, the object released sufficient kinetic energy to generate a shock wave which was heard by people along the French coast closest to the path of the meteor and recorded by French seismographs.

Following its impact, study of 2023 CX1 s orbital track revealed it to be an Apollo-type asteroid, crossing the orbits of Earth and Mars whilst orbiting the Sun at an average distance of 1.63 AU with a period 2.08 years. It last reached perihelion on 13th February 2021, ad would have done so again on March 15th, 2023 had it not swung into a collision path with Earth in the interim.

Continue reading “Space Sunday: asteroid impacts; ISS update”

Space Sunday: rockets, moons, leaks and a ring

The moment of ignition: 31 Raptor motors ignite: Booster 7 during its full static fire test, February 9th, 2023. Credit: SpaceX

SpaceX has completed the largest static fire test for this Starship / Super Heavy launch system, with the 70-metre tall Booster 7 – expected to be part of the first orbital launch attempt – completing a “full duration” 5-7-second test of 31 of its 33 Raptor 2 engines.

The test was made on Thursday, February 9th, amidst on-going work at the orbital launch facilities at the company’s Boca Chica, Texas Starbase site. It had been intended to be full 33-engine test, but one engine was “turned off” during a pause in the countdown at the T -40 second mark, presumably due to an issue being detected, and a second automatically shut down at, or immediately following, ignition.

Even so, the burn was enough for the SpaceX CEO to proclaim the 31 firing engines developed sufficient thrust that, if sustained throughout an 8-minute ascent, it would be enough for Super Heavy to push a fully laden Starship to an altitude where it could reach orbit under the thrust of its six engines.

Ignition came at 21:13:53 UTC, after a partial filling of the booster’s liquid methane and liquid oxygen tanks – Starship 24 had already been destacked from the booster earlier in the month, leaving just the booster on the launch table. Everything appeared to go well, with SpaceX afterwards reporting the engines reached a peak thrust of 7,900 tonnes, or almost twice that generated by the Space Launch System Block 1/1A launcher, and 3,000 tonnes more than the Block 2 SLS cargo launcher.

However, such comparisons need to be put into context: Super Heavy must lift 1200+ tonnes of Starship to low-earth orbit (LEO), carrying 100 tonnes of cargo. SLS is already capable of lifting 95 tonnes of payload to LEO if required, which will increase to 105 tonnes and then 130 tonnes. It is also capable of delivering 27 tonnes to cislunar space, which will increase up to 46 tonnes. The flipside is that Starship and its booster are fully reusable, lowering launch costs; SLS is not. Also, if the booster is not re-used, they Starship could in theory life up to 250 tonnes to LEO; conversely, SLS can reach cislunar space, whereas Starship cannot, not without a complex series of on-orbit refuelling operations.

The test came after extensive work had been carried out at the launch facility after the first two Super Heavy static fire tests (with 7 and 14 Raptor motors respectively) literally stripped the concrete from the base of the launch stand, peppering the launch mount and its surroundings with high velocity cement debris and necessitating extensive repairs to the site.

The problem was one of basic engineering (and frankly, something SpaceX should have considered): the launch table legs and apron underneath the rocket are coated in concrete. A key ingredient of concrete is water, some of which is retained in the concrete as pockets of moisture. Heat concrete to 600°C or more, that moisture flash vaporises into expanding gases, causing the concrete to violently explode.

As I’ve previously noted, this risk is usually negated by the inclusion of a water deluge system which delivers thousands of litres of water to a launch facility, serving a dual purpose: it both absorbs the enormous heat generated by multiple rocket motors by flashing into stream by the force of that exhaust, and it also absorbs the sound waves generated by the motors, further preventing that sound being deflected back up against the rocket and potentially damaging it at launch.

Following the 14-engine test, SpaceX replaced the concrete at the launch facilities with a type designed to withstand very high temperatures. At the time of writing, it is not clear how well this mix withstood the engine test, however the test came at a time when SpaceX is – belatedly – attempting to install a water deluge system to work alongside the existing (and minimal) sound suppression system already part of the launch table.

Tanks for a water deluge system arrive at Starbase Boca Chica via barge. Credit: RGV Aerial Photography
Many – including the SpaceX CEO – are proclaiming the way is now clear for an orbital launch attempt to be made in March. However, this actually depends on a number of factors – the most key of which is whether or not the FAA is satisfied that SpaceX has done / is doing enough to ensure its compliance with all 75 remedial actions specified in its Programmatic Environmental Assessment (PEA).

NASA Tests Upgraded RS-25 Motor

The SpaceX static fire test overshadowed NASA’s test of its updated RS-25 engine for the Space Launch System.

The initial four SLS launches utilise a total of 16 refurbished RS-25 motors originally used with the space shuttle system and referenced as the RS-25D. However, beyond Artemis 4, NASA will be switching to a version of the RS-25 which has been extensively updated. Called the RS-25E, it will deliver 30% more thrust; allowing SLS achieve the upper end of its payload capabilities noted above.

The test, which took place at NASA’s Stennis Space Centre in Mississippi, saw a test stand mounted RS-25E motor fire at 111% of its rated thrust for a total of 8.5 minutes – the amount of time the engines would be used in an actual launch.

A single RS-25E under 1!1% of rated thrust during testing at Stennis Space Centre. The great cloud to the left of the test stand is, in part, steam generated from the engine exhaust striking water from the deluge system Credit: NASA

The RS-25E will commence operations with the Artemis 5 mission in 2028. They will operate alongside the new Exploration Upper Stage (EUS) which will also help raise the SLS system’s performance. EUS itself will entire service with Artemis 4.

Image of the Week

The image below is a computer-generated top-down view of Jupiter and the orbits of its (currently) 92 moons. At the centre of the image is Jupiter and (purple) the orbits of its four most famous Galilean moons – Io, Europa, Ganymede and Callisto. Beyond them, predominantly shown in red, are the remaining 88 moons.

A computer model of the moons of Jupiter in their orbits, with the planet at the centre, as seen from overhead. Credit: Scott Sheppard

Until recently, Saturn held the record for the greatest number of moons (82), the majority of which (43) have been discovered by a team led by astronomer Scott Sheppard. However, Sheppard’s team have also been busy over the years seeking moons orbiting Jupiter – racking up and impressive 70, including the most recent batch of 12 which handed the moon record back to the largest planet in the solar system.

The newest moons were discovered over a period of observations by Sheppard and his team using a number of observatories around the world across 2021 and 2022. They range in size from 1 to 3.2 km across. Most have very large orbits, with nine having periods of more than 550 days. None have been named as yet, as all are awaiting further independent verification.

Continue reading “Space Sunday: rockets, moons, leaks and a ring”

Space Sunday: propulsion, planets and pictures

An artist’s impression of a lunar base using the micro nuclear reactor (NMR) currently being developed by Rolls Royce. Three of the reactors can be seen in the right foreground, casting palm tree like shadows (the “palm frond” shadows are actually the reactors’ radiator panels). Three more of the reactors can be seen in the centre of the image. See below for more. Credit: Rolls Royce Aerospace

In my previous Space Sunday, I covered some of the renewed interest in nuclear propulsion for space missions – and it certainly is a hot topic (no pun intended). Just 24 hours after that article was published, NASA and the US Defense Advanced Research Projects Agency (DARPA) announced they had signed an interagency agreement to develop a nuclear-thermal propulsion (NTP) concept.

Referred to as the Demonstration Rocket for Agile Cislunar Operations (DRACO), the three-phase programme will look to develop and enhance an NTP propulsion system capable of operating between Earth and the Moon and eventually Earth and Mars, potentially enabling fast transit times to the latter measured in weeks rather than months. Nor is this simply a computer modelling exercise: the agencies plan to fly a demonstrator of the propulsion unit in early 2027.

As I noted in my previous piece, NTP uses a nuclear reactor to heat liquid hydrogen (LH2) propellant, turning it into ionized hydrogen gas (plasma) channelled through engine bells similar to those seen in chemical rockets to generate thrust. As I also noted, NTP for space vehicle propulsion is not new; both the US and the former Soviet Union both pursued NTP projects in the early days of the space race – most notably for the US with the Nuclear Engine for Rocket Vehicle Application (NERVA) project, successfully tested on the ground in 1963/64.

A conceptual rendering the DARPA-NASA nuclear thermal propulsion (NTP) test vehicle the agencies hope to fly in 2027. Credit: DARPA

Per the agreement, NASA’s Space Technology Mission Directorate (STMD) will lead the technical development of the nuclear thermal engine, which will be integrated into a vehicle built by DARPA, with that agency leading the overall programme as the contracting authority. Both agencies will collaborate on the overall design of the engine.

DARPA and NASA have a long history of fruitful collaboration in advancing technologies for our respective goals, from the Saturn V rocket that took humans to the Moon for the first time to robotic servicing and refuelling of satellites. The space domain is critical to modern commerce, scientific discovery, and national security. The ability to accomplish leap-ahead advances in space technology through the DRACO nuclear thermal rocket program will be essential for more efficiently and quickly transporting material to the Moon and eventually, people to Mars.

– DARPA director Dr. Stefanie Tompkins

Meanwhile, on January 27th, 2023, the UK’s famed Rolls Royce teased details of its own foray into the space-based nuclear power / propulsion systems: the micro-nuclear reactor (MNR), an extremely robust, self-contained nuclear fission plant which could be used to supply power to bases on the Moon or Mars, or used as a core element in vehicle propulsion systems either individually or as multiple units to provide both thrust and system redundancy, if required.

Images suggest the Rolls Royce MNR is roughly 3 metres in length (excluding the heat radiators). Credit: Rolls Royce

Development of the MNR started as a result of a 2021 agreement between the United Kingdom Space Agency (UKSA) and Rolls Royce (RR) to study future nuclear power options in space exploration. However, the design for the unit builds on RR’s decades-long expertise in developing power plants for the Royal Navy’s nuclear submarine squadrons and, more particularly a project the company has been developing since 2015 to develop and build small modular reactor (SNRs) to meet the UK’s energy needs (SNRs are self-contained, less complex and lower cost alternative to current nuclear reactors).

Precise details of the size of the unit and its output have not been revealed, although images released by RR suggest a single MNR is around 3 metres in length. In discussing the system, the company indicated its designs have reached a point where it plans to have a full-scale demonstrator / prototype running by 2028.

The MNR forms a part of a broader space strategy from Rolls Royce, which also includes systems for high Mach propulsion systems (e.g. ramjets) which could be combined with rocket propulsion to reach orbit, and a new generation of radioisotope thermal generators (RTGs) for power generation on robotic explorer craft and surface system on the Moon and Mars. The overall aim of the strategy is to offer space agencies and the private sector the ability to easily integrate selected elements of RR’s product offerings into their space projects and programmes.

A rendering of a crew-carrying vehicle entering Mars orbit and using a series of Rolls Royce MNRs (outlined in blue) as a part of its propulsion and power system. Credit: Rolls Royce

Returning to NASA, as well as considering the nuclear option, the US agency has been researching the next generation of rocket engines – the rotating detonation rocket engine (RDRE) – and on January 24th, carried out a series of sustained ground tests of a prototype unit.

In a conventional rocket motor, fuel is expended by deflagration combustion – fuel and oxidiser are burnt to produce an energetic gas flow which is then directed through exhaust bells to generate subsonic thrust. With rotating detonation, fuel and oxidiser are injected into a circular channel (annulus). An igniter within the annulus then detonates the initial incoming mix, generating a shockwave which travels around the channel, returning to the point of injection.

At this point, more fuel is injected into the channel to be detonated by the existing shockwave. This increases the shockwave’s speed and force, and the cycle repeats over and over, the shockwave accelerating to supersonic speed, generating high pressures which can be constantly be directed out of the channel to form thrust through an exhaust system even as the shockwave maintains its momentum within the channel.

Whilst this may sound complicated, the upshot is that rotating detonation engines (RDREs) theoretically generate around 25% more thrust than conventional rocket motors, which directly translates to greater delta-V being imparted to vehicles departing Earth, so reducing flight times to the Moon and Mars and elsewhere in the solar system. RDEs could also be inherently less complex than subsonic brethren, reducing the mass of a launch vehicle’s propulsion system.

However, there are drawbacks; for example, the very nature of containing the growing force of the shockwave puts an RDRE under tremendous stress and they have been known to explode. They are also incredibly noisy when built at scale.

Both Russia and Japan have experimented with RDRE technology; in 2018, former Roscosmos chief Dmitry Rogozin claimed Russia had successfully developed the first phase of a 2-tonne class of liquid-fuelled RDRE, although this has yet to be substantiated. In 2021, Japan successfully tested a small-scale (112.4 lbf) RDRE in space, using it to propel the upper stage of a sounding rocket.

The NASA test, carried out at the Marshall Space Flight Centre, Alabama, is the first verified test of a full-scale RDRE. The demonstrator motor operated for a total of 10 minutes, reaching peak thrusts of some 4,000 lbf. This is fairly lightweight by rocket standards, but the aim of the test was not just to generate thrust, but to test the engine’s ability to withstand multiple firings and confirm that a copper alloy referred to as GRCop-42 developed by NASA specifically for use in RDRE engines, was up to the task of reducing the stress on the motor by more efficiently carrying the heat generated by the shockwave away from the annulus structure.

While tests with this motor will continue, NASA is now also moving to the construction of a large unit capable of a sustained 10,000 lbf – the same as mid-range rocket motors – to better understand the potential for RDREs to out-perform “traditional” rocket motors. If successful, it could pave the way for RDRE motors capable of match the output of large-scale engines like the RS-25 used by the Space Launch System (SLS) rocket (418,000 lbf).

Continue reading “Space Sunday: propulsion, planets and pictures”

Space Monday – going nuclear

An artist’s concept of a nuclear bimodal crewed transport, which could be used to deliver crews to the Moon or – in just 45 days – to Mars (Earth, the Moon and Mars not to scale). Credit: NASA

In the heydays of the early space race, both the Americans and Russians toyed with various concepts involving nuclear propulsion for human space exploration within the solar system.

In the United States, this work focused on three major areas of study: nuclear pulse propulsion (NPP) – literally exploding atomic bombs behind a space vehicle, propelling it forward, as exemplified by Project Orion; Nuclear-Thermal Propulsion (NTP) – the use nuclear motors in place of chemical rockets either from launch or once in orbit as seen with Project NERVA; and Nuclear-Electric Propulsion (NEP) – the use of nuclear energy to power low-thrust ion propulsion motors.

NPP was effectively (and perhaps fortunately) abandoned over both the fear of fallout from the vehicle’s atomic explosions during its ascent through the atmosphere and the signing of the Partial Test Ban Treaty in 1963. NTP, using a nuclear reactor to heat liquid hydrogen (LH2) propellant to create ionized hydrogen gas (plasma) which can be expelled via engine bells, has continued to be researched, although its use from launch was overruled dues to the radioactive exhaust plume (thus requiring liquid-fuelled rocket to lift the propulsion units to orbit where they might be used), and remains a solid concept for propulsion that could help reduce the journey time to Mars by weeks.

Nuclear-Electric Propulsion (NEP), relies on a nuclear reactor to provide electricity to an ion engine using an inert gas (like xenon) to create thrust (rather than spewing a radiative exhaust). The resultant thrust is less than that of either NTP or chemical propulsion, but it has the advantage of being able to be maintained for far longer periods, potentially allowing a crewed vehicle to gently accelerate to the half-way point to Mars before trying around and using that same thrust to decelerate gently and achieve orbit around Mars. This could cut a 6-month journey to Mars in half.

Experiments in NEP have continued through until recent times, including space-based test; NTP, however, only reached the stage of ground-based testing before being curtailed. However, it has remained the preferred approach to crewed deep-space missions, should nuclear propulsion on crewed vehicles again be seriously considered. The interest is now re-awakening in light of Project Artemis and America’s stated desire to both return to the Moon and reach beyond it to Mars, with a focus on new approaches to methods of propulsion.

One of these new approaches is the rather tongue-twisty Bimodal NTP/NEP With A Wave Rotor Topping Cycle. The “bimodal” references combining NTP fission to generate the electricity required to power a NEP ion engine, while the “wave rotor” effectively meaning a “supercharger” which further compresses the reaction mass to deliver greater power to the NEP. Research into the approach suggests a transit time to Mars could be reduced to just 45 days.

Based on conventional propulsion technology, the most fuel-efficient Mars crewed mission profile offering the longest period for surface exploration is the Opposition Mission. This requires crews to spend between 6 an 9 months each way in transit between the two planets, with a surface stay of up to 23 months. However, a bimodal nuclear propulsion system could both reduce the transit time each way to 45-60 days, allowing crews to spend more time on Mars, whilst also potentially releasing a mission for the 26-month launch windows, enabling a crew to make an emergency return to Earth if required.

A breakdown of a biomodal transport vehicle. To the right, and docked against the Transhab module is an Orion MPCV, used to deliver crews to the vehicle from Earth and return them home at the end of a mission. The TransHab is a 6m diameter living / working module, powered by conventional solar arrays. Aft of this is the Mars descent / ascent vehicle, then the propulsion control module. The centre of the vehicle comprises the fuel tanks (which also help shield the crew vehicles from radiation from the propulsion module). The combined propulsion (NEP / NTP) module is to the left, also housing the Wave Rider “supercharger”). Credit: NASA

As well as propulsion, NASA is looking at ideas using nuclear power systems for long-duration surface missions when solar and wind power cannot be used / relied upon, These include  KRUSTY, the  Kilopower Reactor Using Sterling Technology, a joint venture between the space agency and the US Department of Energy’s National Nuclear Security Administration (NNSA) successfully demonstrated in 2018. Then there is a new take on the hybrid fusion / fission reactor, first selected by NASA for development in 2013 and which has recently seen renewed investigation, and which is now showing promising signs for future use.

Conventional fusion methods generally comprise either inertial or magnetic confinement, using extreme pressure or a powerful magnetic field to compress a fuel such a deuterium (hydrogen-2), forcing fusion to occur. Both require significant energy input and the generation of significant amounts of heat – around 15 million degrees centigrade. As such, both require large, heavy systems and associated cooling – although this hasn’t stopped the likes of Boeing developing concepts for hybrid systems to propel crew-carrying interplanetary spacecraft to rival biomodal NTP / NEP powered craft.

Hybrid fusion / fission utilises high-energy fast neutrons from a fusion reactor to trigger fission in non-fissile fuels. It is still a complex method, but it has the advantage of being capable of of generating multiple fission events from a single neutron, rather than a single reaction per neutron, requiring less fuel feedstock, and as the fuel is non-fissile, output from the reaction is not radioactive. In fact, such a reactor could even use waste from other fission reactions, disposing of it. Even so, the systems required for hybrid fusion / fission reactors have tended to be extensive and mass-heavy, competing directly with bimodal NTP / NEP systems in size, complexity and mass.

The Boeing hybrid fusion-fission crew-rated space transport, 2021. Credit: Boeing Aerospace
However, a team from NASA’s Glenn Research Centre, Ohio, have developed a potential way in which the complexity (and mass) of a hybrid propulsion system could be significantly reduced.

Selected for Phase I development by the NASA Innovative Advanced Concepts (NIAC) programme, the team has focused on the development of a special lattice into which deuterium can be packed in densities around a billion times greater than a within the core of a conventional hybrid reactor. This, combined with the ability of the fusion process to generate multiple fission reactions, means that overall, less deuterium fuel needs to be carried for feeding into the reactor, thus also reducing the mass of all the associated tanks, piping, etc., required to handle it. Further, the nature of system means that reactions can occur at far lower temperatures than a standard bimodal system, further reducing mass and complexity by eliminating much of the thermal control mechanisms and radiator surfaces required to remove the heat needed to generate the fusion reaction, and the heat it also generates.

Continue reading “Space Monday – going nuclear”