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| ID No : | 699 Edit | Title: | COMPASS Final Report: Low Cost Robotic Lunar Lander |
| Summary / Review : | "The COllaborative Modeling for the Parametric Assessment of Space Systems (COMPASS) team designed a robotic lunar Lander to deliver an unspecified payload (greater than zero) to the lunar surface for the lowest cost in this 2006 design study. The purpose of the low cost lunar lander design was to investigate how much payload can an inexpensive chemical or Electric Propulsion (EP) system deliver to the Moon s surface. The spacecraft designed as the baseline out of this study was a solar powered robotic lander, launched on a Minotaur V launch vehicle on a direct injection trajectory to the lunar surface. A Star 27 solid rocket motor does lunar capture and performs 88 percent of the descent burn. The Robotic Lunar Lander soft-lands using a hydrazine propulsion system to perform the last 10% of the landing maneuver, leaving the descent at a near zero, but not exactly zero, terminal velocity. This low-cost robotic lander delivers 10 kg of science payload instruments to the lunar surface." (Author's abstract) |
| Author(s) : |
McGuire, Melissa L.; Oleson, Steven R., [Glenn Research Center] |
| Publication Date: | 2010 |
| Category(s) : |
Transportation / Lunar launch and landers |
| Web URL : |
http://hdl.handle.net/2060/20110004181
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| 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 : | 20110004181 |
| Other Ref # : | NASA/TM-2010-216218, CD-2006-03, E-17199 |
| Submitted by : | MEP |
| Comments: |
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