Concepts, techniques, and results of organized reliability approach toward ballistic missile flight control systems are summarized; description of Guidance System and Flight Control System, developed by Autonetics; first system must operate continuously over extended period of time whereas second system is activated only periodically and for very brief periods of time; predicted design potential of Minuteman, and flight control group for both silo and flight condition; in-house test results are presented.
Minuteman flight control system -- Approach to and results of formal reliability program
Reliability Maintainability Conference -- Tech Papers
Reliability and Maintainability Conference ; 1963 Reliability
1963
8 pages
Aufsatz (Konferenz)
Englisch
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MINUTEMAN FLIGHT CONTROL SYSTEM THE APPROACH TO AND THE RESULTS OF A FORMAL RELIABILITY PROGRAM
SAE Technical Papers | 1963
|Minuteman approach to system reliability
Engineering Index Backfile | 1964
|The Minuteman Approach to System Reliability
SAE Technical Papers | 1964
|"Case" history in minuteman reliability program
Engineering Index Backfile | 1964
|Functional design of minuteman flight control system
Engineering Index Backfile | 1965
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