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Lunar Soil Erosion Physics for Landing Rockets on the MoonTo develop a lunar outpost, we must understand the blowing of soil during launch and landing of the new Altair Lander. For example, the Apollo 12 Lunar Module landed approximately 165 meters from the deactivated Surveyor Ill spacecraft, scouring its surfaces and creating numerous tiny pits. Based on simulations and video analysis from the Apollo missions, blowing lunar soil particles have velocities up to 2000 m/s at low ejection angles relative to the horizon, reach an apogee higher than the orbiting Command and Service Module, and travel nearly the circumference of the Moon [1-3]. The low ejection angle and high velocity are concerns for the lunar outpost.
Document ID
20130011094
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Clegg, Ryan N.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Metzger, Philip T.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Huff, Stephen
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Roberson, Luke B.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
October 28, 2008
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
KSC-2008-266
Report Number: KSC-2008-266
Meeting Information
Meeting: Joint Annual Meeting of LEAG-ICEUM-SRR (2008)
Location: Cape Canaveral, FL
Country: United States
Start Date: October 28, 2008
End Date: October 31, 2008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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