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Task 1, Design Analysis Report: Pulsed plasma solid propellant microthruster for the synchronous meteorological satelliteThermal vacuum design supporting thruster tests indicate no problems under the worst case conditions of sink temperature and spin rate. The reliability of the system was calculated to be 0.92 for a five-year mission. Minus the main energy storage capacitor it is 0.98.
Document ID
19720011126
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Guman, W. J. (Fairchild Hiller Corp. Farmingdale, NY, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-122358
PCD-TR-71-7
FRD-4070
PC145R8000
Report Number: NASA-CR-122358
Report Number: PCD-TR-71-7
Report Number: FRD-4070
Report Number: PC145R8000
Accession Number
72N18776
Funding Number(s)
CONTRACT_GRANT: NAS5-11494
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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