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Apogee motor rocketry reliability improvementsSince 1963, solid propellant apogee motors have been placing satellites into geosynchronous orbits. Major technological breakthroughs are not required to satisfy future mission requirements; however, there is a need to improve reliability to enhance cost effectiveness. Several management test options are discussed. A summary of results and conclusions derived from review of missions, where failure of a solid motor was inferred, and correlation of system factors with failures are reported. Highlights of a solid motor diagnostic instrumentation study are presented. Finally, recommendations are provided for areas of future apogee motor upgrade, which will increase project cost effectiveness by reducing the potential for future flight failures.
Document ID
19750008548
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Behm, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dowler, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Gin, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 15, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JPL-TM-33-714
NASA-CR-142086
Report Number: JPL-TM-33-714
Report Number: NASA-CR-142086
Accession Number
75N16620
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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