The objective of this experiment is to determine the effects of long-term orbital exposure on the materials used in solid-rocket space motors. Specifically, structural materials and propellants from the STAR/PAM-D series motors and the PAM DII/IPSM-II motors will be tested, as well as advanced composite case and nozzle materials planned for future use. The experiment approach is to expose samples of solid-rocket propellant, liner, insulation, case, and nozzle specimens to the space environment and to compare preflight and postflight measurements of various mechanical, chemical, and ballistic properties.
Space Aging of Solid Rocket Materials (P0005)
1984-02-01
Miscellaneous
No indication
English
Space Aging of Solid Rocket Materials
NTRS | 1992
|Space Aging of Solid Rocket Materials
NTIS | 1992
|Space aging of solid rocket materials
NTRS | 1991
|Space Aging of Solid Rocket Materials (Abstract Only)
NTIS | 1991
|Bibliography of Solid Rocket Component Aging
NTIS | 1966
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