Author Topic: NASA Innocentive Challenge: Space Pioneering - Entering with Mars Aligned  (Read 9508 times)

Offline redliox

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The Innocentive project NASA announced is dedicated to Space Pioneering and, specifically, how to support a mission to Mars lasting 500 or more days.  I'm announcing that I'm putting in a submission to this challenge, but also seeking assistance from people more experienced and knowledgeable about systems for Mars.  I'm going to submit my concept, Mars Aligned, with a focus on orbital operations, solar electric propulsion, and setting up a habitat/fuel factory on Mars.

Although it is a long shot, if the submission does win any prize my vow is to donate half of it towards NASASpaceflight.com to make it an even better information hub of spaceflight knowledge that it already is.  As is, I'm putting together a word document elaborating on what could be done to minimize fuel and maximize the equipment sent to Mars using modern tech (such as chemical, electric propulsion) and near-future developments (ISRU, aerocapture).  Anyone who wishes to contribute will be credited for their work with the ultimate reward given to the website itself.  Knowledge of ISRU systems, 'worker'-style robots, SEP, and deployable heatshields would be especially valued.

The Space Pioneering Challenge is here for those curious: https://www.innocentive.com/ar/workspace/challengeDetail/596835?challenge=9933746
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Offline UberNobody

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I think it's a great idea to do this!  Hopefully we can pitch in and iron out the kinks.

From what I've read of your mission plan, I have a couple questions/concerns:

1.  If aerocapture isn't part of the first cargo missions, there may not be enough pressure to develop it at all.  Look at the shuttle as an example.  Once it started flying, any attempt at evolving or changing the architecture was put down because NASA didn't have the budget to do development and operations at the same time.  Even though aerocapture would reduce the cost per mission, extra funding would be needed after operations begin.

Something to consider.


2. Human orbital mission first.
This kind of mission has different requirements for crew health because they stay in space the whole time.  Artificial gravity is pretty much required for a 2-3 year mission.  If you land on Mars, you can put weights into clothing to simulate Earth gravity if needed.  Make sure that this is factored in when considering an orbit only mission.
« Last Edit: 06/09/2015 12:14 am by UberNobody »

Offline redliox

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I'll put down specifics later tonight, although I'll sum up a few things now for my architecture:

1) Robots and habitats land first, uncrewed and via aerocapture; only cargo flights will use aerocapture to play it safe for humans.

2) The first human flight is orbital. They will primarily visit Deimos and areosynchronous orbit, maybe Phobos.

3) There will be a Martian orbital presence, but it is in high not low orbit; akin to Mars Semi Direct but theaim is to give support to the surface not build ISS Mars.
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Offline redliox

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I've finished the initial draft of the project paper.  Additional artwork and pages elaborating on vehicle breakdowns will be added over the next two weeks.  For those interested in helping in the challenge read through and note me if you believe wish you help or have information that would be useful in explaining my architecture.  Feel free to read the Mars Aligned paper and, again, note me if you believe you can help.
"Let the trails lead where they may, I will follow."
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Offline ehb

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A separate acronym section would help the reader that doesn't already know them and doesn't necessarily memorize them at first reading or is scanning the document.

-ehb.

Offline redliox

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A separate acronym section would help the reader that doesn't already know them and doesn't necessarily memorize them at first reading or is scanning the document.

-ehb.

That will be added near the end in addition to reference material.
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Offline Impaler

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I was also planning to put in a submission dealing just with surface habitat construction.  I had kind of gotten the impression that the contest was oriented towards surface systems and that they were not looking for a DRM which is what you have produced.  But 'pioneering' is an awful vague term so who knows.

Online sdsds

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Great idea!

(For me, this link worked better: https://www.innocentive.com/ar/challenge/9933746)
— 𝐬𝐝𝐒𝐝𝐬 —

Offline redliox

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Finished and submitted 'Mars Aligned' to Innocentive's NASA challenge.  Included with it was an refined overview of the Mars Aligned concept, the delta-v needs of an initial orbital visit to Mars, the excellent artwork of our Tea Monster, and a strong emphasis on how orbital and robotic elements would prepare the way for a crewed landing and outpost.  Feel free to have a peak at the finalized document.

The deadline is July 6, so any results should be known later that month presumably.

It was quite stimulating creating something actually "official" rather than "fan" based.  The internet is full of fans and fanatics, but professionals less so.  However this particular forum is a great mix of both, and I would not have been able to create Mars Aligned without your combined experience and resources.  Whatever the result of the challenge, I proudly credit NASAspaceflight for its help in the effort.
« Last Edit: 06/28/2015 07:55 pm by redliox »
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Offline redliox

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I was also planning to put in a submission dealing just with surface habitat construction.  I had kind of gotten the impression that the contest was oriented towards surface systems and that they were not looking for a DRM which is what you have produced.  But 'pioneering' is an awful vague term so who knows.

Correct, although I think they are looking for suggestions on how to maximize surface stays.  As for a DRM, NASA knows it needs a new one considering 5.0 still refers to Ares (certainly uses the jpeg thumbnails of it in charts).  There was no actual requirement for blueprints insisted upon, so this wasn't a challenge for hardcore engineers (of which the NASA variety are actually forbidden from participation).

Considering most of the NASA material they supplied is "fluff" with a few numbers attached, I simply replied in kind with useful suggestions.  Engineers may look over the submitter's materials, but when you think about it they will still bicker behind the scenes of NASA just as they have for decades before alongside the politicians.  All the same they will pick up on ideas; in my case I try to point out how the orbital route around Mars could be made useful while still drawing upon a Mars Semi-Direct architecture.
"Let the trails lead where they may, I will follow."
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Offline Russel

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For me the key words in the challenge are..

"The Solver is asked to describe one or more Mars surface systems/capabilities and operations needed to achieve this goal"

So its definitely focused on Mars surface systems/capabilities. Otherwise I'd be sorely tempted to write up my architecture. I read the docx and Mars aligned does mention the surface mission briefly, generically mentioning ISRU.. but?

I have a few things to say about ISRU also, going into some technical stuff, but as you know my focus is in a permanent but limited (and largely scientific) presence on Mars. I wonder how the people who offered this prize really feel about that?
« Last Edit: 06/29/2015 03:32 pm by Russel »

Offline redliox

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Got a response back from the Innocentive Challenge.  Sadly, knowing it was a long shot, I didn't win anything from it but they gave a response back briefly explaining their decision:

Quote
“This concept recognizes the value of a phased approach to building up a human presence on Mars. However, the reliance on SLS tanks as habitable volume would require significant changes to the design and operation of the SLS, and the technical challenges associated with those modifications were not recognized or considered. Thank you for participating.”

I respect their reasoning, but simultaneously I have to question it because professional engineers already have interest in using SLS tanks for deep space habitats, including for Martian vehicles; refer to these links on that note: http://forum.nasaspaceflight.com/index.php?topic=30609.0 http://forum.nasaspaceflight.com/index.php?topic=28481.msg878692#msg878692

What does everyone here think?
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Offline A_M_Swallow

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I respect their reasoning, but simultaneously I have to question it because professional engineers already have interest in using SLS tanks for deep space habitats, including for Martian vehicles; refer to these links on that note: http://forum.nasaspaceflight.com/index.php?topic=30609.0 http://forum.nasaspaceflight.com/index.php?topic=28481.msg878692#msg878692

What does everyone here think?

Anything is possible but reusing fuel tanks for anything other than fuel tanks or raw materials puts the idea in the square wheel category.

Offline Impaler

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Yea, I'm very skeptical of reusing wet propellant tanks.  You have all kinds of difficulty in purging them, then they need to be outfitted with a huge mass of equipment which has no real means of being secured to the tank wall unless the tank has been heavily modified.  And all of this work just saves you the mass of the pressure vessel which is a few tons, a small fraction of the total mass needed to make a decent habitat.

The flaw is thinking that a space habitat's ratio of structural elements to furnishings is like a house on Earth.   We use lots and lots of lumber and cement and nails and plaster to make the new house, then some beds and table and chairs are your furnishings, they are tiny in comparison to the mass of the house.  Space Habitats are the reverse, the shell is minuscule and the furnishings are massive.

P.S.  My submission for Expanded Polystyrene vaults covered with regolith was shot-down as well.

“Similar constructed-then-buried structures have been suggested before. Insufficient assessment to determine if this proposal has a clear benefit. Thank you for participating.”

I find this to be a bit unfair as I think I demonstrated a huge improvement in fabrication time and safety through the use of large low-density blocks.  Perhaps they expected more comparisons with alternatives.


Offline redliox

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Yea, I'm very skeptical of reusing wet propellant tanks.  You have all kinds of difficulty in purging them, then they need to be outfitted with a huge mass of equipment which has no real means of being secured to the tank wall unless the tank has been heavily modified.  And all of this work just saves you the mass of the pressure vessel which is a few tons, a small fraction of the total mass needed to make a decent habitat.

The flaw is thinking that a space habitat's ratio of structural elements to furnishings is like a house on Earth.   We use lots and lots of lumber and cement and nails and plaster to make the new house, then some beds and table and chairs are your furnishings, they are tiny in comparison to the mass of the house.  Space Habitats are the reverse, the shell is minuscule and the furnishings are massive.

Bear in mind, the tanks themselves aren't 'reused'.  I never was talking about using them ala the 1980s ideas of reusing shuttle fuel tanks to make mega-space stations.  They would be used in the same way spare tanks from Saturn V were used to create Skylab; Skylab is cited as a working example of how pressure vessels from rocketry could be remodeled into habitats since it's literally been done before...and with 1970s technology.


Quote
P.S.  My submission for Expanded Polystyrene vaults covered with regolith was shot-down as well.

“Similar constructed-then-buried structures have been suggested before. Insufficient assessment to determine if this proposal has a clear benefit. Thank you for participating.”

I find this to be a bit unfair as I think I demonstrated a huge improvement in fabrication time and safety through the use of large low-density blocks.  Perhaps they expected more comparisons with alternatives.

Welcome to my world  :P ;)
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Offline A_M_Swallow

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Bear in mind, the tanks themselves aren't 'reused'.  I never was talking about using them ala the 1980s ideas of reusing shuttle fuel tanks to make mega-space stations.  They would be used in the same way spare tanks from Saturn V were used to create Skylab; Skylab is cited as a working example of how pressure vessels from rocketry could be remodeled into habitats since it's literally been done before...and with 1970s technology.


The Skylab transformation was performed ON EARTH. It took an army of workmen. The furnishings had not been made brittle by freezing them to cryogenic temperatures. What they remodelled was an empty box with a few attachment points.

Offline redliox

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Bear in mind, the tanks themselves aren't 'reused'.  I never was talking about using them ala the 1980s ideas of reusing shuttle fuel tanks to make mega-space stations.  They would be used in the same way spare tanks from Saturn V were used to create Skylab; Skylab is cited as a working example of how pressure vessels from rocketry could be remodeled into habitats since it's literally been done before...and with 1970s technology.


The Skylab transformation was performed ON EARTH. It took an army of workmen. The furnishings had not been made brittle by freezing them to cryogenic temperatures. What they remodelled was an empty box with a few attachment points.

Exactly.  I never said fuel tanks would be refitted in orbit or Mars.
"Let the trails lead where they may, I will follow."
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Offline Impaler

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Bear in mind, the tanks themselves aren't 'reused'.  I never was talking about using them ala the 1980s ideas of reusing shuttle fuel tanks to make mega-space stations.  They would be used in the same way spare tanks from Saturn V were used to create Skylab; Skylab is cited as a working example of how pressure vessels from rocketry could be remodeled into habitats since it's literally been done before...and with 1970s technology.


The Skylab transformation was performed ON EARTH. It took an army of workmen. The furnishings had not been made brittle by freezing them to cryogenic temperatures. What they remodelled was an empty box with a few attachment points.

Exactly.  I never said fuel tanks would be refitted in orbit or Mars.

Sorry, he is clearly going off of my initial post which made the error of assuming you were talking wet-workshops.  I find nothing unconventional about a Sky-Lab style conversion, I've even seen very thorough NASA studies on doing "Sky-Lab 2" using SLS upper stage tanks. 

I would say that they are unlikely to be as good in the ballistic and radiation protection as an expandable Bigelow style module, also maybe some chance for NASA to not have to foot the bill for such a Hab if private companies develop it.

The incredulous response from Innocentive made me think you were proposing something radical, but dry workshops aren't radical and would not require modifying the SLS that launches it, so their response makes no sense.

Offline redliox

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I would say that they are unlikely to be as good in the ballistic and radiation protection as an expandable Bigelow style module, also maybe some chance for NASA to not have to foot the bill for such a Hab if private companies develop it.

That I can agree with, although I haven't seen much Bigelow hardware flown in the last few years which casts a hint of doubt (sans the upcoming BEAM module for ISS).  However, if NASA makes a decision to go inflatable in an announcement by the time SLS flies Bigelow would easily have a revival.  I consider it a 50/50 choice, perhaps depending on whether the next batch of NASA management favors outsourcing to commercial or focusing on "in house" hardware (i.e. SLS tank modeling).

The incredulous response from Innocentive made me think you were proposing something radical, but dry workshops aren't radical and would not require modifying the SLS that launches it, so their response makes no sense.

Maybe they were looking for surface equipment more, or something 'more radical' yet somehow simple to build...as if anything in rocket science were truly simple!  :P
"Let the trails lead where they may, I will follow."
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Offline Impaler

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I would say that they are unlikely to be as good in the ballistic and radiation protection as an expandable Bigelow style module, also maybe some chance for NASA to not have to foot the bill for such a Hab if private companies develop it.

That I can agree with, although I haven't seen much Bigelow hardware flown in the last few years which casts a hint of doubt (sans the upcoming BEAM module for ISS).  However, if NASA makes a decision to go inflatable in an announcement by the time SLS flies Bigelow would easily have a revival.  I consider it a 50/50 choice, perhaps depending on whether the next batch of NASA management favors outsourcing to commercial or focusing on "in house" hardware (i.e. SLS tank modeling).

The incredulous response from Innocentive made me think you were proposing something radical, but dry workshops aren't radical and would not require modifying the SLS that launches it, so their response makes no sense.

Maybe they were looking for surface equipment more, or something 'more radical' yet somehow simple to build...as if anything in rocket science were truly simple!  :P

Remember NASA developed the whole inflatable technology (Trans-Hab) and then was forced to sell it off, so to NASA Bigelow products are 'invented here' rather then in their minds being 'outsourced', they would consider Bigelow Aerospace just a manufacturer.

As for what Innocentive wanted, they did explicitly say surface system.  The kicker seems to be that they don't just want a description of the system as in the kind of info in a patent.  They want you to have done their homework for them and 'proven' that the system is viable, cost-effective, better then the industry standard.  All of which seems a unreasonable burden and an abduction of their core job of reviewing ideas, and I think it will lead to only very narrow near-term upgrades to existing systems having a chance.

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