Problems that solid propellant rocket engineer will encounter in designing for long term storage in radiation environment and summary of present knowledge of radiation environment; mechanisms of radiation degradation and its effects on tensile properties of propellant binders; data from program of irradiation of several propellants are presented; properties of 2 of propellants were changed significantly by doses of order of 4×106 rad.
Effects of ionizing radiation on solid rocket motor components
ARS J
ARS Journal ; 32 , n 7 ; p 1050-1059
1962
10 pages
Aufsatz (Zeitschrift)
Englisch
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