Detailed examination of LDEF's frame and the A0178 thermal blankets by the meteoroid and debris special investigations group

Thomas H. See; Jack L. Warren; Kimberly S. Mack; Michael E Zolensky

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NASA NTRS · 19920018001

Detailed examination of LDEF's frame and the A0178 thermal blankets by the meteoroid and debris special investigations group

Thomas H. See·Jack L. Warren·Kimberly S. Mack·Michael E Zolensky

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Abstract

A responsibility of the group is to define the hypervelocity particle environment encountered by LDEF during its stay in low Earth orbit. LDEF's 6061-T6 aluminum frame and the 'Teflon silver-inconel paint' thermal blankets represent large surface areas that were widely distributed around the spacecraft. The results are reported of high resolution scans of approx. 0.36 and approx. 0.31 sq m for the intercostals and thermal blankets, respectively. The findings are in qualitative agreement with existing model predictions that suggest high differential bombardment histories for surfaces pointing into specific directions relative to the velocity vector of a non-spinning platform in LEO. The production rate for craters greater than or = 50 microns in diameter in aluminum and penetration holes greater than or = 100 microns in diameter in thin foil materials differ by more than a factor of 10 between forward and rearward facing surfaces. These are substantial differences that must be considered during the design of future long duration space platforms in LEO.

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Thomas H. See, Jack L. Warren, Kimberly S. Mack, Michael E Zolensky. 1992-06-01. Detailed examination of LDEF's frame and the A0178 thermal blankets by the meteoroid and debris special investigations group. https://ntrs.nasa.gov/citations/19920018001

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