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CONJUGATING BINARY SYSTEMS FOR SPACECRAFT THERMAL CONTROL. APPENDIX C: AEROASSIST FLIGHT EXPERIMENT CARRIER VEHICLE PRELIMINARY STRESS ANALYSIS Final Report

Author(s):
Ingram, J. E. et al. ( Lockheed Missiles and Space Co. )  
Publication title:
NASA Technical Reports(N89)
Pub. Year:
1989
Issue:
NASA-CR-183609
No.:
G3/18 0204313
Pt.:
NAS1.26:183609
Paper no.:
N89-25261
Page(from):
1
Page(to):
426
Pages:
426
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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