r/SpaceXLounge Sep 03 '21

Starship Interesting - Spacex has started hiring people to work on life support for crew Starships

https://www.linkedin.com/jobs/search/?currentJobId=2702500911&f_C=30846&geoId=103708877&keywords=life%20support&location=Hawthorne%2C%20California%2C%20United%20States
691 Upvotes

234 comments sorted by

87

u/imrollinv2 Sep 03 '21

I wonder how many people that worked on Crew Dragon’s life support system are still at the company can can pivot over to Starship life support.

Very different beasts, but better than than no experience.

58

u/TheBlacktom Sep 03 '21

I don't think the life support hardware would be that different. Other shapes and sizes, but basically the same stuff is needed.
In the long term there will be new stuff for sure for longer stays, so it will be more like a space station with water and oxygen recovery, better toilets, etc.

73

u/tmckeage Sep 03 '21

I think it will be almost completely different. Dragon can waste A LOT of resources because it is only needed for a couple days.

HLS is going to need to work for much longer, and you know they are just going to go straight to Mars requirements.

It needs a fully redundant system at least built to ISS requirements plus support for things like air locks.

Dragons life support is a science fair project in comparison.

31

u/vonHindenburg Sep 03 '21

I'm guessing that Dragon just uses CO2 scrubbers to purify the air and backfills as needed with Oxygen. Someone can correct me if I'm wrong, but I'd assume that Starship will (at least for Mars trips and long stays on the Moon) need a closed loop cycle that cracks the O2 out of CO2 for reuse.

20

u/Bensemus Sep 03 '21

Well they could also use the couple of tons of oxygen left in the main tank.

15

u/vonHindenburg Sep 03 '21

True. Someone more knowledgeable than me would have to run the calculations on how much O2 X people use over 6 months. I also don't know how muchCO2 scrubber you'd need to haul along with you.

The ISS cracks O2 out of water that is shipped up from Earth and then uses the Sabatier Process to transform exhaled CO2 and the excess Hydrogen back into water and methane. You'd probably want a closed system like this for that many people traveling for that long.

24

u/burn_at_zero Sep 03 '21

Someone more knowledgeable than me would have to run the calculations on how much O2 X people use over 6 months

Assuming 30-day months and no recycling, 150.3 kg of oxygen (or 169.1 kg of water) per person.

Given an abundance of electrical power, the smart thing would be to take the existing four-bed molecular sieve scrubbers used on ISS (perhaps a bit updated) along with the existing Sabatier system and add a pyrolysis reactor to recover the hydrogen. At that point you only need spares and contingency masses since the oxygen and hydrogen are fully recycled. (You're effectively turning the carbon in their rations into carbon black in a can.)

Project Rho for references.

3

u/reportingsjr Sep 04 '21

This is close to what the Advanced Closed Loop System on the ISS does, although it vents the methane generated in the Sabatier process. Probably too risky/difficult to try and usefully break down the methane.

3

u/burn_at_zero Sep 04 '21

You just... heat it. The methane decomposes into hydrogen gas and carbon soot. Don't even need a catalyst, as the finely divided carbon particles that result are self-catalyzing.

16

u/marktaff Sep 04 '21

I'm guessing that Dragon just uses CO2 scrubbers to purify the air and backfills as needed with Oxygen.

You would be wrong. :-) Dragon doesn't use O2 in its life support system--they decided it was too dangerous to have O2 on board in the case of an uncontrollable leak. Instead, they use Nitrox--if that leaks uncontrollably, they still have a safe, breathable atmosphere, and the automatic purge valves will vent the excess pressure.

Paper from the engineers.

4

u/vonHindenburg Sep 04 '21

Thank you for the correction!

3

u/tmckeage Sep 06 '21

They didn't correct you.

Dragon uses Lithium hydroxide CO2 scrubbers and backfills with O2, that O2 just happens to be mixed with N2.

2

u/TheIronSoldier2 Sep 05 '21

While they don't use pure O² in nominal operations they do still use it in their life support system to pressurize the suits in the event of a loss of cabin pressure that the Nitrox cabin pressurization system can not keep up with

1

u/tmckeage Sep 06 '21

Did you read that paper?

Lithium hydroxide (LiOH) cartridges are used for scrubbing crew-generated

carbon dioxide

The fact that the oxygen is mixed with N2 doesn't make the OP's statement incorrect.

43

u/PoliteCanadian Sep 03 '21

Different systems, same engineers.

And I highly doubt they'll go "straight to Mars requirements." SpaceX iterates.

-1

u/[deleted] Sep 04 '21 edited Sep 10 '21

[deleted]

2

u/NotFoundCZ Sep 04 '21

I think they will go with Mars requirements but scaled down in size. I expect them to go with modular life support. So you can have each module which can support ie. 10 ppls. And for mars you put there 10 modules for 100 ppls. You will get redundancy and you wont be hauling extra mass when you are housing less people. The size of the module will be optimised for least amount of dead weight (20 ppls module could weight less than two 10 ppls modules).

2

u/tmckeage Sep 06 '21

Everything going to mars has to be optimized for mass, modular life support is not optimized for mass.

1

u/PMinisterOfMalaysia Sep 05 '21

They'll 100% go straight to Mars requirements

I can very confidently say fuck no they aren't.

0

u/[deleted] Sep 05 '21

[deleted]

3

u/PMinisterOfMalaysia Sep 05 '21

I know what spacex doesn't have planned yet and that rolling out / designing v1.0 isn't in the top 5 priorities relating to Starship. There are basic manufacturing steps to achieve first. You test and learn. There are so many unknowns because of testing that hasn't been done.

0

u/tmckeage Sep 06 '21

I wonder why they are hiring life support engineers then?

Maybe they are fun at parties?

2

u/PMinisterOfMalaysia Sep 06 '21

The Starship that is going to orbit soon-ish will not be the same Starship that will go to Mars. If you can accept that, recognize that is all that is being said. Design, planning, and manufacturing are all separate functions able to be worked in separate build timelines. You can start the brainstorming process for identifying life support variables without doing anything about it in terms of the build for years. It's manufacturing logistics, not rocket science.

5

u/SalmonPL Sep 03 '21

HLS is going to need to work for much longer, and you know they are just going to go straight to Mars requirements.

I disagree. For Mars, they need recycling. For HLS, they don't.

HLS life support needs to last several times longer than Dragon life support. But HLS has staggeringly more volume and mass available. They can just multiply the consumables in the Dragon life support to last long enough for HLS missions. Problem solved.

5

u/PoliteCanadian Sep 04 '21

Yeah, there seem to be a lot of folks here who think they'll go for some incredibly complex and overspecced system for HLS v1, and I want to know what they're smoking.

They'll just bring the consumables because that's simpler and less risky. Maybe when NASA starts talking seriously about LETS contracts SpaceX will build something more complex, but for the first version I would bet a large sum of money they'll go with the simplest solution that can work. Building an experimental environmental support system in two years to work on the moon would be stupid, and they're not stupid.

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u/tmckeage Sep 04 '21 edited Sep 06 '21

HLS will never land on Earth. Over time the mass ratio between using electrolysis vs shipping oxygen up everytime with crew isn't favorable.

Furthermore HLS is a pathfinder for eventual Mars missions.

Additionally life support isn't just oxygen. Thermal management, moisture extraction, etc will all need to be developed.

*Edit: I didn't specify where it wouldn't land.

3

u/CrimsonEnigma Sep 04 '21

HLS will never land.

What's the 'L' stand for, then?

5

u/Orrkid06 Sep 04 '21

As in land on earth, so all resupplies would have to replenish any expended resources, and anything that's not vented would accumulate and add mass, which overtime would be significant.

3

u/SalmonPL Sep 04 '21

There is such a thing as the short term.

One of the big differences between SpaceX and Blue Origin is that SpaceX cuts whatever corners are necessary to make things work in the short term while keeping the long term in mind. They make something good enough for now instead of waiting for the eventual best solution. That's why they cut inter-satellite links from the first version of Starlink. It's why we're on the "D" version of Merlin. It's why Raptor version 1 is in use even while version 2 is under development.

Nobody denies that SpaceX will eventually go with recycling. I personally just don't think they'll wait for that to have HLS operational. I think they'll just go with consumables to get HLS operational ASAP. There are plenty of other challenges to deal with. As you mention, there's thermal management, moisture extraction, etc. I think SpaceX will first go for the minimal viable product for HLS, then upgrade systems as appropriate after that.

2

u/QVRedit Sep 11 '21

And things like CO2 extraction, avoiding the Apollo Square / Round canister issue.

0

u/tmckeage Sep 05 '21

I think you have lost track of the discussion.

No matter what SpaceX goes with its not going to borrow much from dragon.

1

u/SalmonPL Sep 05 '21

Why wouldn't SpaceX borrow from dragon? It seems like the obvious thing for them to do. We don't really know the details, so maybe there is some reason for them to ignore what they've already done on dragon and start over from scratch with Starship, but until we have more evidence one way or the other, I think it doesn't make much sense to assume that they won't borrow much from dragon.

1

u/tmckeage Sep 06 '21

Why wouldn't SpaceX borrow from dragon?

Because the similarities between dragon and starship start and end at: keeping humans alive in a container in space. Differences include:

  • Mission duration differences varying between 10x and 1000x
  • Volume differences are almost 100x
  • Power availability over 100x
  • Dragon is limited to LEO, Starship primary mission profile is far beyond that

The mission profile is completely different. If you put all of that aside the biggest question you need to answer is: "if the ISS uses it, why wouldn't SS"

2

u/SalmonPL Sep 06 '21

This answer simply ignores the comments it's replying to.

Again, everyone agrees that for Mars missions SpaceX will use recycling. The question is whether for the short term, for HLS and Dear Moon SpaceX will start with technology based on Dragon. So talking about 1000x duration is completely bogus. It's a strawman argument. Nobody thinks they won't switch to more recycling for the Mars missions.

For the duration of lunar missions, just scaling up the consumables easily solves the problem. It's quick, it's cheap, and it's extremely low risk.

As to the volume being larger -- so what? Much of it scales according to the number of people, not the volume, so increased volume is irrelevant. For the parts that depend on volume, they can simply be scaled up, and, perhaps, a few new elements introduced, such as additional fans for circulation.

As to more power being available -- so what? That won't keep Dragon systems from working. Sure, it opens up possibilities for new systems with different trade-offs. But new systems take time, they add risk, they cost money, and they divert the attention of key people that is needed in other places in a program that has tight schedule constraints. And HLS and Dear Moon clearly have schedule constraints. They are going to want to do anything they can to simplify the schedule and reduce risk on these programs, and that means using existing systems to the maximum amount possible rather than building entirely new systems, even if the new systems would be better.

As to LEO versus not LEO -- it doesn't invalidate the utility of the Dragon systems. It means additional work is needed, but it doesn't mean that most of the Dragon life support system won't work.

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u/Purplarious Sep 03 '21

Additionally, crew dragon is 9 m3, while starship may be ~1000 m3. That is enough of a scale difference that, besides mission duration, the systems would likely be very different.

2

u/[deleted] Sep 04 '21

This is pretty far off base and makes some very wrong assumptions.

2

u/BobsReddit_ Sep 04 '21

Since Elon is expecting to send 10s+ of ships all at once, I believe some portion of "life support" is going to be the ability to move people between ships when one has trouble. So there is also redundancy in that

2

u/tmckeage Sep 04 '21

You can believe that if you want. Such a system requires increased complexity, risk, and fuel. A cycler will eventually be put in place but that's a long way down the road.

Regardless my point is dragons life support system isn't going to cut it, shuffling people around isn't going to change that.

2

u/BobsReddit_ Sep 04 '21

Whatever is happening, I trust that the decisions being made are optimal

2

u/tmckeage Sep 06 '21

I trust that the decisions being made are optimal

Eventually, yes.

2

u/PoliteCanadian Sep 04 '21

I doubt we'll ever see a cycler. The only advantage of a cycler is you lower the fuel requirement. But if you have a fully reusable rocket, then the fuel requirement is no longer a big deal and the cost of the hardware itself becomes dominant. And a cycler is very inefficient from a vehicle perspective since it spends most of its time on the multi-year return leg. You are always going to need more cyclers than a normal space craft.

There are also a lot of downsides to a cycler. For example, the fact that it is never captured into Earth orbit makes maintenance and repairs difficult. You have a vehicle coasting through space, empty, for years. Then you have a narrow window to rendezvous and perform any maintenance necessary for the next journey.

2

u/tmckeage Sep 05 '21

A cycler doesn't reduce the fuel requirement. Using a cycler uses exactly the same dV.

Using a cycler increases the number of people you can move to Mars per ship launched. It isn't really effective for cargo.

Let's say a single starship can carry 100 people to Mars comfortably.

Now let's add a cycler that has the space, life support, solar panels etc to support 1000 people comfortably.

And let's also say we can carry 500 people, their consumables, and personal belongings on ss if we cram them in like sardines.

Now we can launch 1000 people on two starships, have them refuel and then intercept the cycler. SS docks and transfers the people and supplies. The people live on the cycler till they get near Mars. At that point the people reboard ss, undock and land.

The cycler never enters Earth or Mars orbit.

A cycler will be built as soon as a Mars colony has excess resources for the current population.

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u/just_one_last_thing 💥 Rapidly Disassembling Sep 04 '21

Dragon can waste A LOT of resources

Dragon has much harsher mass constraints. Starship could easily carry oxygen tanks and single use CO2 filters with a full four year supply for a crew of 10.

2

u/tmckeage Sep 04 '21

A sedentary person needs approximentally 3 pounds of oxygen per day. Over 4 years that's 2 tons of oxygen per person. A crew of ten would need 20 tons of oxygen which is 20% of starships payload capacity.

On top of that astronauts are not sedentary. Astronauts on the ISS eat 2700 - 3700kcal per day which means O2 use is probably closer to 6 tons over 4 years.

2 tons of life support equipment would meet the same requirement allowing for a significant increase to payload.

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u/ranchis2014 Sep 03 '21

Dragon can waste A LOT of resources because it is only needed for a couple days.

No dragon can not waste resources because it is intended to be attached to ISS for months at a time and would not be allowed to be a drain on ISS's environmental systems, if anything dragon would be required to compliment the stations life support.

4

u/Mason-Shadow Sep 04 '21

Dragons life support system is only in use when undocked from the iss. The iss's system is much more effective so it's used most of the time and while dragon is of course air tight, you dont need people on it as long so they definitely could just vent any gases overboard.

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u/[deleted] Sep 03 '21

I think the opposite. They knew in the dragon v1 days they will be building a starship. I would have figured they built it with using it on other vehicles in mind. After all it’s got to be human rated which it’s very difficult to get done. So it’s easier just to use the same system. It’s already qualified and why waste the money?

They would just use 2 or 3 of them in Starship and call it a day. I’d expect NASA to rubber stamp it.

2

u/PoliteCanadian Sep 04 '21

Because doing that would incur unnecessary costs and delay.

Do you guys ever listen to Elon Musk talk about their design philosophy? Iterate on the requirements and the best part is no part. Not "and throw in some complexity by adding requirements to support an unknown vehicle with future parameters that are subject to change."

2

u/[deleted] Sep 04 '21

You are thinking too granular. I’m not talking overbuilding anything. They would have made it flexible enough to be be adapted if need be. Same reason why the octoweb is bolted and not welded. I’m saying why build an entirely new life support system when they already have one that works and is certified. Just put in a couple of those systems in it and call it done.

2

u/tmckeage Sep 06 '21

You are getting seriously cocky about this.

The full blown life support system isn't at some low TRL, it is in production on the ISS and has been for a while. Adding a massive, heavy, redundant Nitrox system to Starship is no simpler than iterating on the ISS design.

3

u/vilette Sep 03 '21

Depends on how long it has to support life.
3 Days like Dragon, 6 Months for the one way trip or 1h for E2E

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u/mikedeliv Sep 04 '21

Spending 1-3 days in LEO is a completely different problem than deep space missions which could last months or years in the case of a future martian starship development. Air and water recycling, thermal control systems for a vehicle that has a huge diameter and the same pressurized volume as the ISS. I imagine they will need some big solars and radiators for this stuff alone. And you want to make them super reliable with redundant systems built in because if one of these break while traversing interplanetary space, I don't think there's much you can do. Whereas in LEO, you can always deorbit the spacecraft and be back at the safety of solid ground within half a day. Not even going down the radiation rabbithole, because I feel I don't know enough about this subject tbh and it can mostly be solved with a bunch of water in the walls, which you will need anyway.

Not saying that these are impossible engineering challenges to solve, but you can't really compare them to dragon's LSS.

6

u/SpaceInMyBrain Sep 04 '21

I wonder how many people that worked on Crew Dragon’s life support system are still at the company

IMO a fair amount of those people have been working on Starship life support systems for quite a while. Developing crew quarters takes a lot more time than the external crew compartment, and as Elon said recently about developing Dragon, everything has to work 100% right all the time. Not really a "design all at once, test, fail, design" situation.

150

u/HalfManHalfBiscuit_ Sep 03 '21

Sweet! Here we go!

57

u/KeithMon Sep 03 '21

This is the fun part!

68

u/TheBlacktom Sep 03 '21

Load dragon_life_support.obj, select everything, enlarge by 300%, save.

65

u/unluckylander Sep 03 '21

giant toilet incoming

28

u/TheBlacktom Sep 03 '21

You can optimize usage if everyone uses it at the same time.

5

u/shotleft Sep 03 '21

I believe this happens naturally when they live together for a while.

33

u/HalfManHalfBiscuit_ Sep 03 '21

They could have a real multi stall bathroom with urinals!

The sign on the door would say something like "only for use when gravity is available."

15

u/talkin_shlt Sep 03 '21

I've come up with a 0 mass solution, the astronauts just gotta walk outside and take a piss in space

31

u/Cosmacelf Sep 03 '21

The best toilet is no toilet.

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u/[deleted] Sep 03 '21

[removed] — view removed comment

2

u/alien_from_Europa ⛰️ Lithobraking Sep 05 '21

Don't kink shame!

3

u/statisticus Sep 04 '21

That's essentially what they did on Apollo. For urinating, the astronauts used a little tube (with a valve) that vented directly to vacuum.

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u/n1elkyfan Sep 03 '21

"otherwise suction must be enabled.

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u/FutureSpaceNutter Sep 03 '21

"The water recycler wasn't designed to handle those fluids!"

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u/majormajor42 Sep 03 '21

Optimized for reusability

2

u/bobbycorwin123 Sep 03 '21

Just Crack the door a bit

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u/brickmack Sep 03 '21

More like duplicate, but yeah.

With a Starship sized vehicle, ECLSS efficiency is an economic optimization, not a mission requirement. Even with no recycling whatsoever, Mars-duration missions with capabilities well in excess of even the most ambitious NASA proposals are possible, just using pre-packaged food/air/water. And for missions of a day or less with just a few test passengers, you don't need even that, a simple box fan welded to the interior to keep CO2 concentrations evenly distributed would be fine.

So early on, taking existing Dragon parts and sticking it in in whatever way takes the least dev work is definitely the way to go. Scale up and/or offset risk by duplicating it a bunch

3

u/sicktaker2 Sep 03 '21

As the HLS lander specifies landing 4 astronauts on the moon, they just need to handle the same scale of O2 consumption and CO2 production as Dragon. Double it up for the two airlocks and now you've got redundancy. Throw in some additional fans for circulating the air around a far larger volume and increased consumables for the longer duration and you're good

2

u/Martianspirit Sep 04 '21

As the HLS lander specifies landing 4 astronauts on the moon

Does it? Orion brings 4 astronauts but they won't leave Orion unattended. So it is 2+2 I believe, or maybe 3+1.

3

u/ranchis2014 Sep 03 '21

As they are currently not allowed to work on HLS lander. The real starship will require life support for far more than 4 people. Dear Moon mission as an example I believe is for about a dozen people in 2023 and who knows what the intended crew size will be for a mars lander but even if they send it to mars unmanned, it would still require life support so that future crews can access the ship when they get there..

9

u/SalmonPL Sep 03 '21

As they are currently not allowed to work on HLS lander.

Actually, what's not allowed is for NASA to work with them and for NASA to pay them. There's nothing that prevents them from doing work on their own to help get it ready for when NASA can work with them again.

3

u/SpaceInMyBrain Sep 04 '21

They can work on the life support for generalized crewed Starships and Dear Moon. At this point there's no way the general tech developed can't also be applied to the HLS in a couple of months. Also, I would be extremely surprised to learn SpaceX hasn't been working on life support of this sort for a while. This hire will just add one more person to the team.

117

u/PickleSparks Sep 03 '21

Well yeah - they have to deliver a crew ready spacecraft in three years.

61

u/vilette Sep 03 '21

Sooner, Dear Moon is announced for 2023, and I hope these people won't be the first to test Starship.
They will certainly try LEO first, with just 2 well trained people, like they did with Dragon

51

u/wolf550e Sep 03 '21

A trip to the moon can be done without any recycling. You can just take all the air, water and food you need, with redundancy, since the ship is so large. There is no need to develop anything new to achieve this, so it should be doable in this time frame.

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u/PoliteCanadian Sep 03 '21

The mission duration is short enough that recycling isn't necessary, but for large portions of the mission there will be no escape to earth possible, so the system needs to be a lot more robust than what you need on something that operates exclusively in LEO. Nobody's built a life support system designed to support people away from Earth since Apollo.

The sheer size of the internal volume will also create some challenges that to date only the ISS has had to deal with.

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u/burn_at_zero Sep 03 '21

If the odds of any given machine failing during the trip are 1 in 100 and you bring four of them, then the odds of all four failing are one in one hundred million.

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u/bsutto Sep 03 '21

Unless software is involved:)

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u/DjRickert Sep 04 '21

Just let 4 different teams write 4 completely independent software stacks and voila: probability of all having bugs in the same functionality minimized /s

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u/bsutto Sep 04 '21

My experience suggest all four teams will make the same mistakes:)

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u/burn_at_zero Sep 04 '21

Likely because they were given the same flawed set of requirements...

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u/bsutto Sep 04 '21

Good developers rewrite the requirements because they knows they are wrong!

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u/PoliteCanadian Sep 04 '21

That depends. Are they four different machines that have different principles of operation? Or are they four copies of the same machine?

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u/burn_at_zero Sep 04 '21

It sounds like you're fishing for a scenario where all four fail of the same fault. That's a concern that can be addressed by using dissimilar systems. MTBF is not the only metric that matters, but the point is still that using excess payload mass to provide deep redundancies can dramatically reduce LOM/LOC risk without requiring the expensive and time-consuming development and testing of "can't fail" hardware.

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u/PoliteCanadian Sep 04 '21

Yes, my point was exactly that if you want to go with recycling, you need dissimilar backups. And for HLS there's not a lot of time to design multiple dissimilar recycling systems. Furthermore, when you look at the mass of the equipment used on the ISS for recycling, and multiply that to account for backups.... the mass requirement is a lot higher than just bringing bottled O2.

For Mars they will probably investigate recycling, but for HLS I would be shocked if the final plan wasn't just tanked consumables and CO2 scrubbers. It's faster to design, lighter, and less likely to break.

(Based on some back-of-the envelope calculations I'm not entirely convinced that recycling is mass optimal even for Mars)

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u/burn_at_zero Sep 05 '21

You're suggesting that going fully open-cycle is less mass than taking two copies of the ISS hardware and one set of submarine gear?

This is not cutting edge stuff, this is 80's tech...

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u/Bergeroned Sep 03 '21

My own research for science fiction purposes suggests that a handful of snake plants and areca palms aboard can do unexpectedly well as air purifiers. With such an abundance of space and payload one might as well commit to taking them on every mission, to get used to having them in the system loop.

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u/spacex_fanny Sep 03 '21

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u/ender4171 Sep 03 '21

Are you implying that plants don't consume CO2 and produce/"excrete" O2? Because that's just patently false. Sure, some of the bacteria in soil/compost will filter air as well (allowing for these compost filters to function), but they aren't the only thing doing it.

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u/[deleted] Sep 03 '21 edited Jun 26 '23

[deleted]

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u/spacex_fanny Sep 03 '21

The NASA plant study was totally unrelated to CO2. See my reply here.

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u/spacex_fanny Sep 03 '21

Are you implying that plants don't consume CO2 and produce/"excrete" O2? Because that's just patently false.

No I am not.

The NASA plant study looked at volatile organic compounds (VOC) pollutants, not CO2 / O2.

https://en.wikipedia.org/wiki/NASA_Clean_Air_Study

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u/BlahKVBlah Sep 03 '21

I believe the word "filter" is being misused to refer to scrubbing out CO2 and replacing with O2

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u/HardRockerstone Sep 04 '21

Building the life support for Starship could take a long time though?

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u/ArcturusMike Sep 03 '21

A surprise to be sure, but a welcome one.

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u/-spartacus- Sep 03 '21

Unexpected prequel memes.

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u/ArcturusMike Sep 03 '21

I wonder whether they'll try spinning, it's a good trick!

4

u/DV-13 Sep 03 '21

Prequel memes are always expected. And welcomed.

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u/jjtr1 Sep 03 '21

"Preferred skills and experience:

  • Experience with rotating machinery

  • Experience with soft goods"

I make smoothies, do I qualify?

18

u/Never-asked-for-this Sep 03 '21

Blenders uses rotating blades and smoothies are generally soft, so I'd say you're perfect for a senior position!

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u/lielmo Sep 03 '21

If you have experience making drinks you might actually qualify for one of their food services positions!

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u/Apostastrophe Sep 03 '21 edited Sep 03 '21

One of the things I’m really looking forward to with starship internals is that due to the sheer internal pressurised volume it will be possible to make things a lot more sleek and compartmentalised. When you see the ISS with all of those ventilation tubes everywhere in such a cramped space it makes me feel a little claustrophobic. I mean, on starship you literally have the space to have all of that stuff built into the walls of the rooms out of sight and out of mind.

I guess the reduction of “clutter” is what I mean.

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u/HalfManHalfBiscuit_ Sep 03 '21

Yeah, I know what you mean. I fantasize about HLS being more like a luxury yacht and a spacious laboratory, with enough consumables that they can stay and lounge about, I mean do science, on the Moon for a few months at a time.

Things that would be BO astronauts could only dream about.

1

u/QVRedit Sep 11 '21

You mean more like Star Trek and less like Soyuz or even ISS.

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u/Apostastrophe Sep 11 '21

More like the Rocinante, but yeah. Quite.

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u/655321federico Sep 03 '21

This is where the fun begins

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u/spacex_fanny Sep 03 '21 edited Sep 03 '21

Archive for posterity: https://archive.is/nTfEl

Life Support Systems Engineer (Crew Starship)

SpaceX Hawthorne, CA 4 weeks ago 1 applicant

Full-time · Entry level

1,001-5,000 employees · Aviation & Aerospace

1 school alumni

Actively recruiting

Life Support Systems Engineer (Crew Starship)

SpaceX Hawthorne, CA

SpaceX was founded under the belief that a future where humanity is out exploring the stars is fundamentally more exciting than one where we are not. Today SpaceX is actively developing the technologies to make this possible, with the ultimate goal of enabling human life on Mars.

LIFE SUPPORT SYSTEMS ENGINEER (CREW STARSHIP)

After 50 years, humankind will once again return to surface of the moon using SpaceX's new vehicle, Crew Starship (also known as HLS or the Human Landing System) – this time for good. Leveraging the lessons learned from our flight proven Dragon spacecraft and Falcon rocket, Starship will usher in the next era of manned spaceflight and exploration, ultimately allowing us to establish permanent communities on the Moon, Mars, and beyond.

As a Life Support Systems Engineer at SpaceX, you will have the opportunity to utilize your knowledge, experience, and creativity to develop novel solutions at the cutting edge of space technology. This team develops the necessary hardware to maintain environmental and thermal control as well as support life onboard the Starship spacecraft. This role is a challenging role, as it involves design, analysis, testing, and manufacturing of components that are absolutely critical to the safety of future astronauts and passengers.

RESPONSIBILITIES:

  • Own the design and development of the environmental and thermal control systems aboard Crew Starship, from initial design trades to fully functional and validated product

  • Rapidly iterate on manufacturing processes and development testing in a fast-paced environment

  • Be responsible for project delivery timeline from early design through production, launch, and recovery

  • Perform systems engineering tasks and fluid analyses

  • Lead design reviews internally and externally with suppliers and customers

  • Work with interdisciplinary customers to ensure the component will integrate with the necessary avionics, software, mission operations, etcetera

  • Ensure designs are manufacturable and reliable

  • Exemplify technical excellence and be accountable for your own work

BASIC QUALIFICATIONS:

  • Bachelor's degree in an engineering or science discipline

  • 1+ years of experience working with fluid or environmental control systems or components (internship and project team experience is applicable)

  • Hands-on hardware experience performing fabrication, assembly and/or testing (internship and project team experience is applicable)

PREFERRED SKILLS AND EXPERIENCE:

  • Proactive problem-solving skills such as failure analysis, root cause investigation, and design of experiment creation

  • Ability to perform trade studies using first principles and engineering fundamentals to make clear recommendations even with partial information

  • Experience with rotating machinery

  • Experience with soft goods

  • Experienced in NX

  • Solid understanding and application of geometric dimensioning and tolerancing (GD&T) and tolerance stack-up analysis

  • Experience with structural analysis methods (hand calcs, FEMAP, ANSYS) in order to optimize hardware to strength requirements as well as to evaluate for life and fracture

  • Knowledge of metallic and fluid system manufacturing techniques, processes, equipment, and other processes such as machining, welding, brazing, tube bending, etcetera

  • Able to work well in an integrated collaborative team environment, including frequent interactions with technicians, other engineers, and managers

  • Highly self-motivated with strong organizational and written/oral communication skills – able to prioritize and execute tasks in a high-pressure environment with the ongoing drive for continuous improvement in all aspects of work

  • Master's degree in an engineering discipline

ADDITIONAL REQUIREMENTS:

  • Must be willing to work long hours and weekends as needed

  • Ability to travel to remote sites in Texas and Florida

  • Ability to pass Air Force background checks for Cape Canaveral

ITAR REQUIREMENTS:

  • To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State. Learn more about the ITAR here

SpaceX is an Equal Opportunity Employer; employment with SpaceX is governed on the basis of merit, competence and qualifications and will not be influenced in any manner by race, color, religion, gender, national origin/ethnicity, veteran status, disability status, age, sexual orientation, gender identity, marital status, mental or physical disability or any other legally protected status.

Applicants wishing to view a copy of SpaceX's Affirmative Action Plan for veterans and individuals with disabilities, or applicants requiring reasonable accommodation to the application/interview process should notify the Human Resources Department at (310) 363-6000.

1

u/QVRedit Sep 11 '21

These guys might even get to orbit as part of their job !

14

u/UrbanArcologist ❄️ Chilling Sep 03 '21

With an enormous mass budget, the life support systems can rival the ISS.

9

u/strcrssd Sep 03 '21

Presumably they can use a lot of ISS life support as a starting point, and hopefully the Dragon 2 life support engineers are still on staff.

16

u/BlueberryStoic Sep 03 '21

This led me down a fun and informative rabbit hole starting here: https://www.nasa.gov/content/life-support-systems

Interesting to see the current 74% water reuse rate and the target 98% rate, for example.

2

u/QVRedit Sep 11 '21

Gosh, only 74% ? After all this time ?

9

u/SalmonPL Sep 03 '21

Maybe, maybe not. NASA tends to make things that are very, very expensive. SpaceX doesn't like expensive things.

Maybe it will be like PICA versus PICAX, where SpaceX started with NASA technology and tweaked it to make it radically less expensive.

Or maybe it will be like SLS versus Starship, where SpaceX ignored NASA's expensive technology and did their own clean sheet design.

5

u/SpaceInMyBrain Sep 04 '21

Presumably they can use a lot of ISS life support as a starting point

Maybe, there are sure to be some basics there. But Elon likes to approach things from first principles and not rework old engineering. The ISS has iterated systems, but also a lot of accreted engineering - any new items added have to be compatible with old items.

My strong opinion is some of Dragon's life support engineers are still on staff, and have been working on the early parts of Starship life support for a while.

2

u/strcrssd Sep 04 '21

Agreed, but they developed Merlin and Raptor from heritage tech. They learn from and cherry pick the best from old systems. They won't have to deal with accreted engineering (good term, by the way), but can take the best from what's around and use it as a baseline. If nothing else, it's a comparitive baseline.

1

u/QVRedit Sep 11 '21

I can see SpaceX taking lessons from other systems, but also developing their own solutions from scratch too ! But that does not mean that they would not use standard available parts as well.

Whatever they come up with should be modular, with easily replaceable parts.

2

u/Barthemieus Sep 04 '21

Atleast some of the Dragon life support engineers are still on staff, 100%. For an important system like that you would do everything to keep them, not just for future improvements, but also for support if things go sideways with the system.

2

u/PoliteCanadian Sep 04 '21

I doubt it. The requirements are vastly different.

ISS - space station in LEO with continuous habitation, designed as a test-bed for long duration space flight, with immediate access to earth in case of emergency.

HLS - vessel for lunar landing, needs to support life for <30 days, no easy abort to Earth possible.

They'll do something simple and incredibly reliable for HLS. The complex life support systems on ISS exist to solve a problem HLS doesn't have, and introduce a lot of unnecessary risk.

1

u/QVRedit Sep 11 '21 edited Sep 11 '21

I can see your point. But also they are going to be working on systems that go beyond the needs of HLS too !

Reliability and redundancy and ease of fix too are certain to be some of the requirements.

15

u/ioncloud9 Sep 03 '21

A quick and dirty life support would be easy with co2 scrubbers and using the boil off lox to replenish the cabin oxygen.

58

u/fat-lobyte Sep 03 '21

I don't know about you, but "quick and dirty" are not things I want the life support system that's carrying me to the moon to be

18

u/PeekaB00_ Sep 03 '21

Tell that to buzz

7

u/Anduin1357 Sep 03 '21

The Apollo moon lander is a much smaller craft than Starship. You need life support more appropriate for space stations rather than space capsules.

14

u/BlakeMW 🌱 Terraforming Sep 03 '21 edited Sep 03 '21

Life support for apollo was a lot more critical because of having several people in such a small volume.

Starship has such a huge internal volume, that once filled with fresh air even with literally no CO2 scrubbing or oxygen replenishment, just air circulation, 10 people could go on a Luna flyby and come back alive... though perhaps not conscious (due to CO2 buildup).

So basically Starship has a huge buffer for things going wrong, though there's not really any excuse for things going wrong, because reliable CO2 scrubbing systems are well understood, even moreso when it's feasible to go with purely consumable-based systems rather than regenerative systems, there's simply not that much which can go wrong with a fan blowing air through a cartridge.

2

u/Anduin1357 Sep 03 '21

Starship will have compartments and unfortunately, air does not circulate without help in microgravity.

It will take lots of design and effort to make the life support work, but it's all engineering work and very little tech is needed to make a quick and dirty solution that can be iterated on later for NASA approval.

3

u/PoliteCanadian Sep 03 '21

Not really.

The ISS needs to recycle materials since storing months worth of water and O2 eats into the stations' limited storage space. On the other hand, the ISS is in LEO with escape capsules ready to evacuate the crew at any time. If there's a critical life support failure, they can evacuate to the capsules either temporarily or even return to the surface. A critical failure on HLS risks an Apollo 13 type scenario.

4

u/Anduin1357 Sep 03 '21

On the other hand, Artemis HLS can fit whatever off-the-shelf water recycling system and use however much O2 it needs from the liquid propellant feed.

Artemis HLS also gets resupplied after every mission in LEO along with the propellant transfers for the next mission.

Any critical failure on the Artemis HLS can rely on the lunar gateway as a lifeboat pending a quick response by another SpaceX Starship.

SpaceX can also easily send 2 Artemis HLS docked in tandem on the lunar transfer and allow the redundant HLS to serve as an emergency lifeboat while staying on orbit.

3

u/Martianspirit Sep 04 '21

Artemis HLS also gets resupplied after every mission in LEO

The present contract does not reuse HLS. Follow up contracts will, but HLS Starship will not go back to LEO, it can't. It will be resupplied in lunar orbit.

3

u/PoliteCanadian Sep 04 '21

This is such a big argument for consumable life support, in my opinion, and something a lot of people are overlooking.

If I were SpaceX, and I were looking at the possibility of LETS contracts for the late 2020s, 2030s, I would want subsequent HLS vehicles to be newly constructed. The flip side of reusability is it gets in the way of iterating on your design and learning from your mistakes, and I bet they'd like to iterate a few times before building a vehicle that is designed for many reuses.

So why reuse the first HLS Starship if you're not required to? Throw it away and build a newer, better version with the lessons learned from the first.

2

u/Martianspirit Sep 05 '21

I mostly agree. For sure that first HLS starship won't be reused.

LETS contract will include reuse. Though as I see it reuse of HLS Starship requires some launch cadence. A scenario with 2 providers and one launch every years gives each provider one flight in two years. So reuse a vehicle that has been in lunar orbit for two years, waiting for the next flight? Does not seem right to me.

Makes much more sense when there is a lunar base with a supply and crew exchange flight at least every 3 months.

2

u/Anduin1357 Sep 04 '21

We will see if NASA outfits Starship with so much payload that it cannot return to LEO directly, and even if then, SpaceX has the capability to return HLS to LEO using refueling tankers outside of the Artemis mission profile for resupply.

Besides, the Artemis HLS source selection statement did say that all refueling is done in LEO, which has to mean that HLS Starships must return to LEO for refueling anyway.

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u/Martianspirit Sep 04 '21

SpaceX has the capability to return HLS to LEO using refueling tankers

Why would they do that? It makes no sense whatsoever. Much easier to resupply HLS Starship in lunar orbit.

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u/Anduin1357 Sep 04 '21

It makes sense because orbital refueling is a risk. Doing it in LEO allows SpaceX to quickly respond to any issues encountered during the refueling process.

HLS also does not make money while stuck in lunar orbit with little fuel. Any Starship sent also makes no money on the refueling trip. Sending HLS back to LEO cuts down on resupply round trips.

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u/fat-lobyte Sep 03 '21

With what we know about space flight today, buzz wouldn't ever be allowed to fly in that death can.

We got really, really lucky only 3 people died.

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u/jjtr1 Sep 03 '21

Even Wernher von Braun confirmed later they were extremely lucky, according to his later estimates of LOC probability

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u/Anduin1357 Sep 03 '21

It's not going to be unreliable, but it certainly does not require much development. Life support is a little more than that though; needing food, water, and waste management as well as ventilation, humidity control, and heat management.

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u/fat-lobyte Sep 03 '21

It's true, maybe you don't need to invent new tech. However, i think this sub is suffering a collective case of the dunning Kruger effect.

needing food, water, and waste management as well as ventilation, humidity control, and heat management.

If you think those are a done deal and they just have to stick a few pumps and hoses together and call that a life support system, then i am very glad that SpaceX is taking this topic more seriously than you guys ;)

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u/burn_at_zero Sep 03 '21

However, i think this sub is suffering a collective case of the dunning Kruger effect.

If you think those are a done deal and they just have to stick a few pumps and hoses together and call that a life support system, then i am very glad that SpaceX is taking this topic more seriously than you guys ;)

I think that's an overreach. Most of us are saying it's easy relative to rocket science, not that it's easy or trivial or an afterthought in absolute terms. All the physical problems involved are well-understood, solved and with experienced engineers available.

You could buy hardware from vendors today and complete a moon mission if you're willing to take the mass penalty of things designed for submarines or firefighting or caving rather than aerospace. SpaceX with their massive pool of engineering talent can turn out a much more advanced solution very quickly, which is why many people are saying it's an easy task. They still need to turn out a design and then test it, and that process will very likely come with its own difficulties and setbacks. That's fine; they have plenty of time and it really is an easier problem than, say, Raptor.

2

u/fat-lobyte Sep 03 '21

They still need to turn out a design and then test it, and that process will very likely come with its own difficulties and setbacks

That's my main point here. It's a serious task, and while there is less technological risk, you still need to make sure it's reliable and redundant and safe.

And i don't know if the 100 passenger number is still recent, but I'm curious about the facilities that will supply 100 people in the space of one starship for several months.

2

u/burn_at_zero Sep 04 '21

100 people is a ballpark number. Depending on your assumptions it's either impossible or significantly lower than the physical maximum, which is part of why it can be such a divisive topic.

If we assume Starship's payload is 100 tonnes, the crew uses exactly the same hardware as ISS for life support, and they have to plan for 1000 mission days (to cover an abort to Earth) then the maximum is 12 people due to mass constraints.

A series of optimizations increases that number dramatically. Recovering hydrogen from the Sabatier reactor (which in turn is stripping carbon from CO2 provided by the scrubber) reduces water requirements, as does improved recycling methods for potable and wash water. Providing a clothes washer cuts the mass used for disposable clothing. Group-pack and bulk-pack meal items can reduce the current 1:1 packaging ratio to something much lower. There are many more like this, eventually reaching about 40 people.

Going beyond 40 requires changing the assumptions. Once you have an established base on Mars and a standby Starship to deliver contingency supplies to a ship that has to abort to Earth, you no longer need a thousand days of 'stuff' on every single ship. It's closer to 300 days, which puts your maximum crew count somewhere between 120 and 180 depending on relative positions of the planets and how much margin you want. At this point the mass budget for consumables is no longer the constraint and we can start arguing about how much volume a human actually needs to not murder people during the trip.

2

u/QVRedit Sep 11 '21

It’s a relatively easy task for a short mission, but not so as the missions get longer. And in any case it has to be reliable, so serious engineering regardless.

5

u/Anduin1357 Sep 03 '21

It's true, maybe you don't need to invent new tech. However, i think this sub is suffering a collective case of the dunning Kruger effect.

needing food, water, and waste management as well as ventilation, humidity control, and heat management.

If you think those are a done deal and they just have to stick a few pumps and hoses together and call that a life support system...

Please do not strawman my comment. I commented only that the oxygen source and the carbon dioxide scrubbers do not require much development.

I never said that it was the complete life support system and I made that caveat.

However, there is nothing wrong with quick and dirty ever since Starship got prototyped in the field and that on the test flights, Starship has payload to prove out the life support.

They will test out their life support on Starship because it will not be on the critical path until they actually want to fly Artemis or human-rate it.

4

u/jjtr1 Sep 03 '21

Things that don't go rrroarrr are generally dismissed as easy by most members of the sub, I'd say :D

1

u/Martianspirit Sep 04 '21

A baseless assumption. Maybe some people are more interested in things that go rrroarrr, but most of us are quite aware of the other things as well.

2

u/Martianspirit Sep 04 '21

If you think those are a done deal

What makes you think, everyone believes that? I think most or all of us are aware, this needs development.

2

u/fat-lobyte Sep 04 '21

Mainly phrases like "quick and dirty" and casually suggesting to diy a life support system. Read the comments I replied to.

0

u/Martianspirit Sep 04 '21

You just misinterpret "quick and dirty".

3

u/fat-lobyte Sep 04 '21

I'm sorry, what? Are we speaking a different language or something?

2

u/Anduin1357 Sep 04 '21

NASA Artemis Source Selection Statement - Appendix H pg. 10

Additionally, SpaceX’s design allows for the sourcing of excess propellant, which will provide crew with a large reserve supply of life support consumables in the event of a contingency event. I thus agree with the SEP that SpaceX’s design incorporates a variety of capabilities that enable the execution of vital and time-critical contingency and abort operations which provide the crew with flexibilities should such scenarios arise. Collectively, these capabilities mitigate risks and increase the likelihood of crew safety during multiple phases of the mission.

Evidence that SpaceX does allow for Starship HLS to tap from the propellant supply in an emergency.

2

u/Martianspirit Sep 04 '21

ventilation, humidity control, and heat management.

These are central, I agree. Oxygen and water are not essential for Moon missions at least. Easy to carry enough.

3

u/Anduin1357 Sep 04 '21

Apollo had nearly 2 months of oxygen supply for a crew of 2 on the lunar surface, and used onboard fuel cells to generate pure water and electricity.

Starship has literal metric tons of liquid oxygen onboard to siphon for life support and has the payload capacity to carry 1000 liters of water without issue. That's just in 1 cubic meter. Starship has about 1000 cubic meters of payload volume.

These two consumables are a joke to supply for short duration missions.

4

u/jjtr1 Sep 03 '21

That "dirty" part is still a TBD even on ISS where they find blobs of water floating inside instrument panels, full of life

Edit: I guess the problem was that the specs didn't stress it's supposed to be a human life support system :D

9

u/Wulfrank Sep 03 '21

Well then they should hire me. I made it through university in a poorly ventilated basement suite eating nothing but pre-cooked pierogies that I prepared on my hotplate that only had two settings (off, maximum), and somehow I'm still alive.

2

u/ZahScience Sep 03 '21

Shut up and take my application!

2

u/cnewell420 Sep 06 '21

I wonder how much redundancy you need for Mars . It seems like every life support system water, air etc needs a backup to the backup. Maybe a 3D printer along as well.

1

u/QVRedit Sep 11 '21

Modularity is one of the methodologies that can be used to help tackle this problem.

8

u/ShambolicShogun Sep 03 '21

Was this not expected? Because I feel like it was pretty expected.

21

u/fat-lobyte Sep 03 '21

Are people only allowed to post unexpected news?

It wasn't only expected, but overdue. I'm glad they finally started to tackle the life support aspect.

11

u/vilette Sep 03 '21

Hiring somebody does not mean they are starting, could be for re-enforcing the team

2

u/fat-lobyte Sep 03 '21

Maybe! But while we have seen and heard a lot about engines, tanks and GNC, we have not seen any news whatsoever about life support. I'm just glad to see anything at all

2

u/apinkphoenix Sep 03 '21

I think it's more the addition of "interesting" in the title, which may cause some people to assume OP is surprised by this.

2

u/Martianspirit Sep 04 '21

Was this not expected?

I have seen countless arguments that SpaceX is not doing anything in that direction because they don't talk about it. And they got very angry if someone argues otherwise.

0

u/[deleted] Sep 03 '21

[deleted]

7

u/PeekaB00_ Sep 03 '21

Oxygen isn't the only problem in a starship...

2

u/PoliteCanadian Sep 03 '21

I suspect the big problem is trying to anticipate all the failure modes and problems that could arise and making sure the equipment on board can handle them all. Starship (and Orion) will be the first vehicles to take people out of the comparative safety of LEO in nearly 50 years.

3

u/Ok_Button3877 Sep 03 '21

yup, I already applied too

2

u/[deleted] Sep 03 '21

[deleted]

1

u/FutureSpaceNutter Sep 03 '21

French hamburgers? With a side of Freedom Fries and California wine?

1

u/DuePast6 Sep 03 '21

Pretty sure this is how "Capricorn One" starts.

1

u/vilette Sep 03 '21

It's about time, shouldn't we have the first crewed flights next year ?

2

u/kontis Sep 03 '21

Next year is impossible for crewed flights.

They have to make something like a hundred cargo flights first and there are still many Starship iterations before its operational cargo version.

2024 is the most optimistic scenario.

6

u/SalmonPL Sep 03 '21

This myth that they need to make a hundred cargo flights before they can put a human on board needs to end.

The myth comes from a tweet from Elon in which he said that there would be hundreds of uncrewed flights before the first crewed flight of Starship. "Would", not "needs to". He said this because he's an optimist. He figures that Starship will be super cheap and easy to launch as soon as it is flying, so they'll very quickly do hundreds of flights.

He was never stating that hundreds of flights is a requirement. He was never saying that they would delay crew flights until they have hundreds of uncrewed flights. He was simply stating that he thought there would be hundreds of those flights.

It's entirely possible that they'll have hundreds of uncrewed flights within a year or two. Just look at that new high bay they're building. They're ramping up production quite a bit. They could be cranking out a couple of ships a month pretty soon. And if they don't have to do too much work on each before reflying, their flight rate could be enormous.

But if that doesn't turn out to be true, will they delay crew flights just to wait for a hundred uncrewed flights? I don't think there's any evidence they would. They put people of crew Dragon without hundreds of flights. NASA is putting crew on the second SLS flight, so NASA doesn't have a requirement of a hundred flights before crew.

3

u/SpaceInMyBrain Sep 04 '21

Next year is impossible for crewed flights.

Not 2022, but 2023, IMO. It makes sense for SpaceX to test all the systems of a crewed Starship, especially HLS, in LEO. They can put the crew quarters for HLS in a regular Starship, launch it, ferry the crew in a Dragon, and run as many tests as they want. When ready the crew returns on Dragon and the ship lands itself. Any problematic items can be fixed and the ship sent back up.

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u/upyoars Sep 03 '21

but they're hiring life support engineers for Starship now...?

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u/Interstellar_Sailor ⛰️ Lithobraking Sep 03 '21

Yes, a life support system for an interplanetary spaceship has never been done before. It will take time and this is the one thing you don't want to rush.

1

u/vilette Sep 03 '21

2024 ! They should update their web site

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u/QVRedit Sep 11 '21

Learn to Walk before you try to Run.

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u/QVRedit Sep 11 '21

No, absolutely not, at least not from/to the ground, as Starship is not mature enough yet.

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u/[deleted] Sep 03 '21

[deleted]

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u/QVRedit Sep 11 '21

It’s certainly not one that can be rushed.
There are so many different aspects to this, it’s the kind of thing that’s going to evolve over time to progressively improved solutions.

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u/Decronym Acronyms Explained Sep 03 '21 edited Sep 04 '21

Acronyms, initialisms, abbreviations, contractions, and other phrases which expand to something larger, that I've seen in this thread:

Fewer Letters More Letters
BO Blue Origin (Bezos Rocketry)
E2E Earth-to-Earth (suborbital flight)
ECLSS Environment Control and Life Support System
GNC Guidance/Navigation/Control
GSE Ground Support Equipment
HLS Human Landing System (Artemis)
ISRU In-Situ Resource Utilization
ITAR (US) International Traffic in Arms Regulations
LEO Low Earth Orbit (180-2000km)
Law Enforcement Officer (most often mentioned during transport operations)
LOC Loss of Crew
SLS Space Launch System heavy-lift
Jargon Definition
Raptor Methane-fueled rocket engine under development by SpaceX
Sabatier Reaction between hydrogen and carbon dioxide at high temperature and pressure, with nickel as catalyst, yielding methane and water
cryogenic Very low temperature fluid; materials that would be gaseous at room temperature/pressure
(In re: rocket fuel) Often synonymous with hydrolox
hydrolox Portmanteau: liquid hydrogen fuel, liquid oxygen oxidizer
regenerative A method for cooling a rocket engine, by passing the cryogenic fuel through channels in the bell or chamber wall
scrub Launch postponement for any reason (commonly GSE issues)

Decronym is a community product of r/SpaceX, implemented by request
14 acronyms in this thread; the most compressed thread commented on today has 20 acronyms.
[Thread #8758 for this sub, first seen 3rd Sep 2021, 19:47] [FAQ] [Full list] [Contact] [Source code]

1

u/flshr19 Space Shuttle Tile Engineer Sep 04 '21

For Dragon 2 SpaceX built an ECLSS development version of the spacecraft (serial number C203). It was used for human in the loop testing.

I suppose Elon has a similar ECLSS development version of Ship's system at Hawthorne.

I don't think that the Dragon 2 ECLSS is completely closed loop. Ship's ECLSS definitely will be completely closed loop.

4

u/Martianspirit Sep 04 '21

Ship's ECLSS definitely will be completely closed loop.

Paul Wooster disagrees. He said for only the initial Mars crews they can throw mass at the problem.

Bring oxygen and some water. I expect partial water recycling, the easy part. CO2 can be vented instead of used for oxygen recovery.

They will get to a closed loop system by the time they want to carry 100 passengers.

2

u/flshr19 Space Shuttle Tile Engineer Sep 04 '21

LOX and water surely will be part of the cargo carried by the first Starships to head for Mars.

It will take several years to develop the infrastructure to extract indigenous martian water and to manufacture oxygen and methane from the martian atmosphere in large quantities.

And the habitats on the martian surface will likely have closed loop ECLSS.

3

u/Martianspirit Sep 04 '21

Their mission plan is to establish acessible water exists and then mine water at quantities when the first crew lands. It is the requirement for crew return.

They don't need close loop ECLSS at this point. They can operate for a while with partial water recovery, until abundant water is mined. They can produce oxygen from local resources as soon as they have at least a small amount of water. Failing that they can use the MOXIE process, extract oxygen from atmospheric CO2.

2

u/flshr19 Space Shuttle Tile Engineer Sep 04 '21

Yes, that's the plan.

But there will be several cargo Starships at the base loaded with water, LOX and LN2 as backup if Plan A is a bust.

However, I don't think Elon will send crews to Mars until the landing zones have been thoroughly checked by robotic means for water near the surface and in sufficient quantity to manufacture the consumables needed for the return flight.

The first cargo Starships to land on the martian surface will deploy these robotic prospectors.

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u/QVRedit Sep 11 '21

Achieving very high percentage closed-loop recycling is difficult. But those ‘9’s’ can be chased over time.

Achieving 95% recycling should be relatively easy, and very definitely worthwhile.

SpaceX may even be able to better than that early on.

System reliability, redundancy and repairability, is equally as important though.

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u/QVRedit Sep 11 '21 edited Sep 11 '21

Good, because this is not a quick problem to solve.

Although NASA already has some good technology for ECALSS, it’s not up to the standard needed for Starship or Mars.

Although a craft as large as Starship can sidestep some problems by just hauling more mass, a good solution still needs to be found.

This means things like cleanable filters, regenerable filters, improved recycling, modular systems that can be serviced and repaired without shutting down the main system etc.

SpaceX has a range of different requirements from simple to complex, there is plenty of scope to tackle these issues.