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Meteoroid bumper experiment on Explorer 46The effectiveness of a meteoroid bumper in reducing meteoroid penetrations is discussed. The bumper reduced the penetration flux by a factor of 30 and demonstrated a weight savings of a factor of 6.9 in the material needed to resist meteoroid penetration. The method of calculating the penetration flux recommended in the NASA space vehicle design criteria for meteoroid damage assessment was found to be very conservative, and changes are suggested. The optimum distribution of material between a bumper and the main wall is discussed.
Document ID
19810020617
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Humes, D. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
L-14329
NASA-TP-1879
AD-A277032
Report Number: L-14329
Report Number: NASA-TP-1879
Report Number: AD-A277032
Accession Number
81N29155
Funding Number(s)
PROJECT: RTOP 506-55-13-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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