A program was conducted in which the response and failure charactersitcs of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program. (Author)
Simulated Air Launch Environment, Volume II. Aeroheat Data Summary
1974
317 pages
Report
Keine Angabe
Englisch
Simulated Air Launch Environment. Volume 1
NTIS | 1974
|NTRS | 1982
|NTIS | 1978
|NTRS | 1981
|NTIS | 1980
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