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Apollo Lunar Module Landing GearThe Apollo lunar module landing-gear flight-performance results and three principal gear development problems are discussed. In evaluating the lunar module touchdown performance, strut stroking and toppling stability are the prime factors and are governed primarily by touchdown velocity and surface slope at the touchdown point. Flight results are shown to be well within design values, and the landing-gear has performed successfully in all landings.
Document ID
19730010151
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rogers, W. F.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Publication Information
Publication: The 7th Aerospace Mech. Symp.
Subject Category
Space Vehicles
Accession Number
73N18878
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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