Search | Add a publication |
ID No : | 832 Edit | Title: | Altair Lander Life Support: Requirements Analysis Cycles 1 and 2 |
Summary / Review : | "Life support systems are a critical part of human exploration beyond low earth orbit. NASA's Altair Lunar Lander has unique missions to perform and will need a unique life support system to complete them. Initial work demonstrated a feasible minimally -functional Lander design. This work was completed in Design Analysis Cycles (DAC) 1, 2, and 3 were reported in a previous paper'. On October 21, 2008, the Altair project completed the Mission Concept Review (MCR), moving the project into Phase A. In Phase A activities, the project is preparing for the System Requirements Review (SRR). Altair has conducted two Requirements Analysis Cycles (RACs) to begin this work. During this time, the life support team must examine the Altair mission concepts, Constellation Program level requirements, and interfaces with other vehicles and spacesuits to derive the right set of requirements for the new vehicle. The minimum functionality design meets some of these requirements already and can be easily adapted to meet others. But Altair must identify which will be more costly in mass, power, or other resources to meet. These especially costly requirements must be analyzed carefully to be sure they are truly necessary, and are the best way of explaining and meeting the true need. If they are necessary and clear, they become important mass threats to track at the vehicle level. If they are not clear or do not seem necessary to all stakeholders, Altair must work to redefine them or push back on the requirements writers. Additionally, the life support team is evaluating new technologies to see if they are more effective than the existing baseline design at performing necessary functions in Altair's life support system." (Author's abstract) |
Author(s) : |
Anderson, Molly; Curley, Su; Rotter, Henry; Yagoda, Evan, [Johnson Space Center] |
Publication Date: | 2010 |
Category(s) : |
Transportation / Lunar launch and landers Life / Mobile Life Support (PLSS, LSHS) / Vehicle |
Progress Type: | AD ( A=Analysis only, D=Design, T=Testing, C=Completed or Commercial product ) |
Web URL : |
http://hdl.handle.net/2060/20100019169
If this link is broken, please Add Comment below. We try to keep author contact details, and a backup copy in our offline library. |
PERMANENT code(s) : | L,U |
(Explanation of the last 3 rows above) |
In the row above, there are up to 4 possibilities: U = URL you can click on to get a copy instantly from another source on the internet, or request it from that source D = Downloadable from PERMANENT (such as because no other URL known...) L = LAN copy, PERMANENT has a digital copy but not downloadable from our website P = Paper copy in the PERMANENT office Typically, only 0 to 3 methods are available. |
NTRS : | 20100019169 |
Other Ref # : | JSC-CN-20582 |
Submitted by : | MEP |
Comments: |
Please add your thoughtful Comments to this paper after reading it. All comments are reviewed and approved before being posted publicly below. If you wish to submit a private comment to the curator, instead of a public comment, just write "Private" at the start of your comment. Corrections and suggested additions to our records are appreciated. |
Add Comment |