NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Meteoroid, and debris special investigation group preliminary results: Size-frequency distribution and spatial density of large impact features on LDEFAll craters greater than or equal to 500 microns and penetration holes greater than or equal to 300 microns in diameter on the entire Long Duration Exposure Facility (LDEF) were documented. Summarized here are the observations on the LDEF frame, which exposed aluminum 6061-T6 in 26 specific directions relative to LDEF's velocity vector. In addition, the opportunity arose to characterize the penetration holes in the A0178 thermal blankets, which pointed in nine directions. For each of the 26 directions, LDEF provided time-area products that approach those afforded by all previous space-retrieved materials combined. The objective here is to provide a factual database pertaining to the largest collisional events on the entire LDEF spacecraft with a minimum of interpretation. This database may serve to encourage and guide more interpretative efforts and modeling attempts.
Document ID
19920014071
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
See, Thomas H.
(Lockheed Engineering and Management Services Co., Inc., Houston TX., United States)
Hoerz, Friedrich
(POD Associates, Inc., Albuquerque NM., United States)
Zolensky, Michael E.
(POD Associates, Inc., Albuquerque NM., United States)
Allbrooks, Martha K.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Atkinson, Dale R.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Simon, Charles G.
(Institute for Space Science and Technology, Inc., Gainesville FL., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA. Langley Research Center, LDEF: 69 Months in Space. First Post-Retrieval Symposium, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
92N23314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available