Author Topic: NASA/ESA - Mars Sample Return mission  (Read 332975 times)

Online StraumliBlight

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1060 on: 04/04/2025 06:57 pm »


Richard French (Rocket Lab) discusses their Mars Sample Return architecture.

Offline thespacecow

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1061 on: 04/05/2025 05:47 am »
He's more qualified than 99% of the person here.

It's funny some people here claim if you don't work in the industry then you're automatically "wrong", yet when I quote from people actually in the industry right now (instead of 20 years ago), the objection changed to "no, he's not in the right field..."

I can’t speak to what other folks have told you in the past.  But whatever they wrote doesn't change the fact that Lee is a planetary scientist who made his bones calculating cratering rates, not an aerospace engineer who made his bones calculating mass fractions.

Yes, you know when aerospace engineers actually examined Starship for MSR? It's when NASA assembled the review team to examine MSR industry studies, and after review they accepted Starship as an option for MSR. Yet you dismissed that as well. So you don't listen to Mars scientists, you don't listen to aerospace engineers, who do you think we should listen to anyways...



Quote from: VSECOTSPE
1. When I advocated refueling the Starship lander in Mars orbit, it's not even in the context of doing MSR.

Yes, it was.  You quoted this from another poster at the start of your post 390 in the other thread where you discussed refueling Starship in Mars orbit with another Starship.  They were explicitly discussing the “context of MSR”.

People keep talking about starship in low Mars orbit. How would that be helpful in the context of MSR?

Per the study source selection, refueling Starship in Mars orbit was never part of the SpaceX study for MSR.

You have no idea what the context even is.

Post #379 from @matthewkantar is not talking about Starship launched from Mars surface to LMO and waiting for refueling, he's talking about the - now been proven to be wrong - idea from @TheRadicalModerate (and some other person who shall remain unmanned) that Starship cannot land on Mars due to PP, so it can only be used as a transit stage to bring lander to LMO, this is articulated in post #343: "Just think of it as a really big launcher, with an expendable second stage, capable of delivering a lot of mass to LMO for roughly the same launch and refueling costs as if you used a directly launched FHE, VC6-H, or New Glenn."

Post #379 is asking why having Starship - arriving from Earth - in LMO is helpful to MSR, this is pretty clear if you actually read his next sentence: "Once braked into orbit I’m fairly sure Starship would need to be topped up to go anywhere.", you don't brake into LMO when launching from Mars, you brake into LMO when arriving at Mars from Earth.

Then in post #380 Eric Hedman stated that Starship landing on Mars surface can bring a bigger MAV, which @matthewkantar replies in post #381 that "I agree. Post after post above have suggestions Starship in LMO. I was addressing that.", which further proves the context of discussion is that Starship as transit stage and stopping at LMO is useless to MSR, and their proposal is to use Starship as a Mars lander to bring bigger MAV for MSR.

So in summary, none of these have anything to do with refueling a Starship launched from Mars surface at LMO.




Quote from: VSECOTSPE
That's not using round-trip human Mars missions to retrieve MSR samples, it's using unmanned test landing and takeoff - which precedes human Mars mission - to do MSR. The takeoff part is basically the same thing as SpaceX's proposal of using Starship as MAV.

But that’s not what you proposed.  In post 590 in the other thread, you wrote that this was the same as your post 74 in that thread.  And in post 74, you argued for using Starship to do the entire MSR mission, same as a manned Mars Starship mission or an unmanned precursor:

Just use a uncrewed version of your crewed Mars architecture to do MSR. You're going to have to do uncrewed test flight of this architecture anyway, so adding sample return is just a bonus...

Remember the US moon rocks were also brought back by a crewed architecture, albeit via crewed mission instead of uncrewed mission.

Again, per the study source selection, SpaceX never proposed replacing MSR with an unmanned dry run of their manned Mars Starship architecture.

Of course they proposed replacing MSR with an unmanned dry run of their manned Mars Starship architecture, they proposed using Starship as MSR Mars lander and potentially as MAV, which is literally a unmanned dry run of their manned Mars Starship architecture, since manned Mars Starship will need to land on Mars too, and it needs to be able to take off from Mars too. Having unmanned Starship doing these for MSR is a test flight of the manned Starship architecture, whether they actually spelled this out in their proposal is irrelevant.
« Last Edit: 04/05/2025 05:53 am by thespacecow »

Online VSECOTSPE

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1062 on: 04/05/2025 10:57 am »
Yes, you know when aerospace engineers actually examined Starship for MSR? It's when NASA assembled the review team to examine MSR industry studies, and after review they accepted Starship as an option for MSR. Yet you dismissed that as well.

I doubted your claim that SpaceX had proposed, and NASA had accepted, the use of Starship for all MSR mission segments.  That’s not the same thing as dismissing Starship as an option for MSR.

You have no idea what the context even is.

I just quoted your quote of the earlier poster, where they literally and explicitly wrote that the context is MSR:

People keep talking about starship in low Mars orbit. How would that be helpful in the context of MSR?

Of course they proposed replacing MSR with an unmanned dry run of their manned Mars Starship architecture, they proposed using Starship as MSR Mars lander and potentially as MAV, which is literally a unmanned dry run of their manned Mars Starship architecture,

An unmanned dry run of the manned Mars Starship architecture would bring Starship back to Earth.  Per the source selection, SpaceX never proposed that.  They only proposed using Starship for launch, the transit to Mars, the landing, and maybe (in parentheses) the ascent.

Over at least the several posts I’ve pointed out (and I’m sure there’s more), you supported, advocated, insisted on (whatever the verb is) the former.  That was never in the cards.  Per the source selection, SpaceX only proposed the latter.

Online VSECOTSPE

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1063 on: 04/25/2025 01:17 pm »

Isaacman weighs in:

Quote
Asked by the committee’s chairman, Sen. Ted Cruz (R-Texas), if the Mars Sample Return program should be “outsourced to industry,” citing a proposal to do so from Rocket Lab, Isaacman offered a one-word response: “Yes.”

https://spacenews.com/isaacman-calls-potential-nasa-science-cuts-not-optimal/

Offline Jim

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1064 on: 04/25/2025 06:12 pm »

He's more qualified than 99% of the person here.

It's funny some people here claim if you don't work in the industry then you're automatically "wrong", yet when I quote from people actually in the industry right now (instead of 20 years ago), the objection changed to "no, he's not in the right field..."


No,a planetary scientists are not in the "industry".  They may know a lot about instruments, something about spacecraft and little about launch vehicles.

Offline Blackstar

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1065 on: 04/30/2025 08:26 pm »

Offline deltaV

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1066 on: 05/01/2025 04:32 pm »
[slides]

The first of those slides is labeled "Douglas-Bradshaw", which I'm guessing is MSR Program Director Donya Douglas-Bradshaw. The first, third and fourth slides are labeled "4/30/25". Were all four slides presented by Donya Douglas-Bradshaw on April 30?

Offline Turnbill

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1067 on: 05/04/2025 04:03 pm »
Trump budget forfeits Mars Sample Return to China


Offline Kaputnik

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1068 on: 05/09/2025 03:30 am »
I'm old enough to remember when Skycrane was first mooted for MSL
It seemed crazy, but the complexity kind of made sense when landing a rover- no separate platform needed, no egress ramps, reuse the rover's wheels as the landing gear. Very smart, really.

I'm surprised that it still makes sense when landing a static platform. Is it just a case of using the highest performance heritage system, despite it originally being designed for a very different mission?
Does Skycrane bring other benefits for MSR over a conventional lander?
"I don't care what anything was DESIGNED to do, I care about what it CAN do"- Gene Kranz

Offline Robotbeat

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1069 on: 05/09/2025 01:06 pm »
The fact that it is the largest demonstrated landing method for Mars helps.
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Offline Kaputnik

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1070 on: 05/09/2025 04:31 pm »
The fact that it is the largest demonstrated landing method for Mars helps.

Yes I understand that is the main reason. I've read that the heritage MSL design would have to be scaled up by about 20% to accommodate MSR. Which is almost exactly what needed to be done when the Pathfinder system was scaled up for MER. That turned in to an almost complete redesign. There has to be a risk that the same would happen with Skycrane, and if you're going to do that much development, why not just switch to a more conventional lander platform?

Obviously smarter people than me have decided that an enlarged Skycrane makes the most sense. I'm just wondering if there are other, technical, advantages, rather than the heritage argument.

Of course in the current budgetary environment it's likely all moot.
"I don't care what anything was DESIGNED to do, I care about what it CAN do"- Gene Kranz

Offline JulesVerneATV

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1071 on: 05/10/2025 11:17 am »
After billions of dollars in spending and decades of planning, NASA may be forced to abandon precious samples of air, rock and soil on the Martian surface.

https://www.scientificamerican.com/article/trump-budget-calls-for-stranding-nasas-mars-samples-on-the-red-planet/

Quote
the White House’s Office of Management and Budget (OMB) dropped a budgetary bombshell, proposing to cut NASA’s top-line funding by a quarter, slash the space agency’s science budget by nearly half and entirely eliminate MSR. The cancellation is justified, the OMB document claims, because MSR is “grossly overbudget” and its goals of sample return will instead “be achieved by human missions to Mars.”

Offline jstrotha0975

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1072 on: 05/10/2025 02:59 pm »
This is what I've been saying all along, no point of an MSR mission if we are sending humans to Mars anyway.

Offline Don2

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1073 on: 05/10/2025 07:25 pm »

Yes I understand that is the main reason. I've read that the heritage MSL design would have to be scaled up by about 20% to accommodate MSR. Which is almost exactly what needed to be done when the Pathfinder system was scaled up for MER. That turned in to an almost complete redesign. There has to be a risk that the same would happen with Skycrane, and if you're going to do that much development, why not just switch to a more conventional lander platform?

Obviously smarter people than me have decided that an enlarged Skycrane makes the most sense. I'm just wondering if there are other, technical, advantages, rather than the heritage argument.

Of course in the current budgetary environment it's likely all moot.

My hypothesis is that there are subtle and very difficult to solve problems in the 'conventional' approach that uses a rocket powered descent and landing legs.  I suspect that there are very complicated interactions between the lander, the legs, the exhaust plumes and the ground which make the conventional approach hard.

When the mass of the MAV increased JPL did try to design a much larger conventional lander. The effort failed when it became apparent that they had badly underestimated the mass of the landing legs.

I would also point out that engineers have gone to great lengths to find alternatives to the conventional approach. Despite the success of Viking, they used airbags for the MER rovers and the skycrane for MSL. I would remind you that Viking, at $8 billion in today's money, was the most expensive planetary science mission in history. My guess is that most of that cost went to developing the landers and the EDL system rather than the orbiters. JPL has been living off that Viking legacy for decades. Significantly heavier landers than MSL need very expensive new supersonic parachutes and aeroshells which increase the cost. The diameter of the MSL aeroshell is already close to the 5m limit set by current rocket fairings so scaling it up is not a simple task.

For all those reasons they need to design a sample return lander that is no heavier than Perseverance. Like you, I am a little uncomfortable with the proposal to make it 20% heavier. Perhaps the skycrane system can be up rated by 20% but there is a risk there.

Offline Don2

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1074 on: 05/10/2025 07:52 pm »
This is what I've been saying all along, no point of an MSR mission if we are sending humans to Mars anyway.

I'd point out that there is no significant money for a man to Mars program in the 'skinny' budget. There is $1 billion in funding which is enough for a few design studies but that is an order of magnitude less than what a serious manned Mars effort requires even if you are very optimistic about how cheaply SpaceX can do it. They added $113 billion to defense so the money was there for a manned Mars program if the will was there to do it.  The political system obviously has no interest in funding it...ever.

Returning the samples would require sending humans to Jezero Crater. Landing thousands of kilometers away in another part of Mars won't do. Jezero is higher and colder than landing sites along the equator so a manned landing might want to go somewhere else.

A manned landing would also contaminate the area with organic molecules which would make analysis of the samples harder and could potentially obscure evidence for Martian biology.

Offline Kaputnik

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1075 on: 05/11/2025 01:43 am »

My hypothesis is that there are subtle and very difficult to solve problems in the 'conventional' approach that uses a rocket powered descent and landing legs.  I suspect that there are very complicated interactions between the lander, the legs, the exhaust plumes and the ground which make the conventional approach hard.

This didn't seem to trouble the LEM very much, and it was far bigger.

Quote
When the mass of the MAV increased JPL did try to design a much larger conventional lander. The effort failed when it became apparent that they had badly underestimated the mass of the landing legs.
Sure, but even a payload delivered via Skycrane needs to sit on something. The beauty of using it for a rover is that you reuse the wheels as the landing legs.

Quote
I would also point out that engineers have gone to great lengths to find alternatives to the conventional approach. Despite the success of Viking, they used airbags for the MER rovers and the skycrane for MSL.
MER was a product of the almost paranoid reaction to the back to back losses of MPL and MCO. NASA pivoted towards maximum risk reduction, and adopted the 'cheap and simple' MPF landing system, and even flew twin spacecraft, something which hadn't been done since Viking a quarter of a century earlier.
Airbags are not the most mass efficient way of delivering a payload, but they are a pretty foolproof option (it sucks when your lander falls over). The USSR used a basically similar idea and succeeded in landing the first probe on the moon this way, despite a general technology base that was far behind the USA.

MSL invented Skycrane as a way of optimising the delivery of a rover.

Neither proves that conventional 'platform' landers have been abandoned.
What did NASA select when they last landed a static payload? They went with the conventional approach, and Phoenix was the result.
« Last Edit: 05/11/2025 02:03 am by Kaputnik »
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Offline Robotbeat

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1076 on: 05/11/2025 01:58 pm »
This is what I've been saying all along, no point of an MSR mission if we are sending humans to Mars anyway.

I'd point out that there is no significant money for a man to Mars program in the 'skinny' budget. There is $1 billion in funding which is enough for a few design studies but that is an order of magnitude less than what a serious manned Mars effort requires even if you are very optimistic about how cheaply SpaceX can do it. They added $113 billion to defense so the money was there for a manned Mars program if the will was there to do it.  The political system obviously has no interest in funding it...ever.

Returning the samples would require sending humans to Jezero Crater. Landing thousands of kilometers away in another part of Mars won't do. Jezero is higher and colder than landing sites along the equator so a manned landing might want to go somewhere else.

A manned landing would also contaminate the area with organic molecules which would make analysis of the samples harder and could potentially obscure evidence for Martian biology.
Starship can do it. Initial mission for the same price as Artemis 4.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

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Offline Robotbeat

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1077 on: 05/11/2025 02:07 pm »
Starship is getting $1 billion for a dozen launches and Starship HLS for Artemis 4. This is around the same needed for a couple one-way mars launches.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

To the maximum extent practicable, the Federal Government shall plan missions to accommodate the space transportation services capabilities of United States commercial providers. US law http://goo.gl/YZYNt0

Offline DanClemmensen

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1078 on: 05/11/2025 02:19 pm »
Starship is getting $1 billion for a dozen launches and Starship HLS for Artemis 4. This is around the same needed for a couple one-way mars launches.
The HLS Option B contract is $1.13 Billion, but this includes development of the Option B HLS in addition to the Artemis 4 mission. I don't know How SpaceX internally allocates that money between the development and the mission. I also have no idea how many tankers they used to compute the price. The number of tankers has shifted around a lot since the contract was negotiated before being awarded in March 2022.

Offline Robotbeat

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Re: NASA/ESA - Mars Sample Return mission
« Reply #1079 on: 05/11/2025 07:28 pm »
You do have an idea. 8-20 tankers. That’s an idea.
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

To the maximum extent practicable, the Federal Government shall plan missions to accommodate the space transportation services capabilities of United States commercial providers. US law http://goo.gl/YZYNt0

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