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Mission Design for the Lunar Pallet LanderMarshall Space Flight Center is developing a small lunar lander capable of delivering up to 300 kg of payload to the lunar surface near the North or South Pole. Originally designed as a lander for a small rover, the Lunar Pallet Lander, has seen several design iterations over the last couple of years. This paper will cover how the vehicle and mission design changed from being a co-manifested payload candidate in NASA’s Space Launch System to its current design, which could be launched with an Evolved Expendable Launch Vehicle (EELV), and reach a wide range of polar landing sites.
Document ID
20190001933
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Craig, A. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Holt, J. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hannan, M. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Orphee, J. I.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
March 27, 2019
Publication Date
January 13, 2019
Subject Category
Lunar And Planetary Science And Exploration
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS 19-330
M18-7143-1
Report Number: AAS 19-330
Report Number: M18-7143-1
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Ka''anapali, HI
Country: United States
Start Date: January 13, 2019
End Date: January 17, 2019
Sponsors: American Astronautical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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