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BALLIST: A computer program to empirically predict the bumper thickness required to prevent perforation of the Space Station by orbital debrisA computer program called BALLIST that is intended to be a design tool for engineers is described. BALLlST empirically predicts the bumper thickness required to prevent perforation of the Space Station pressure wall by a projectile (such as orbital debris) as a function of the projectile's velocity. 'Ballistic' limit curves (bumper thickness vs. projectile velocity) are calculated and are displayed on the screen as well as being stored in an ASCII file. A Whipple style of spacecraft wall configuration is assumed. The predictions are based on a database of impact test results. NASA/Marshall Space Flight Center currently has the capability to generate such test results. Numerical simulation results of impact conditions that can not be tested (high velocities or large particles) can also be used for predictions.
Document ID
19940009647
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rule, William Keith
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
BER-550-248
NAS 1.26:193825
NASA-CR-193825
Report Number: BER-550-248
Report Number: NAS 1.26:193825
Report Number: NASA-CR-193825
Accession Number
94N14120
Funding Number(s)
CONTRACT_GRANT: NAS8-38555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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