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Hybrid resistojet development Final reportHigh specific impulse of several hydrazine thrustors ignited by electrical heaters within thrust chamber during experimental evaluation
Document ID
19710015761
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
January 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
AVSD-0083-71-RR
NASA-CR-118322
Report Number: AVSD-0083-71-RR
Report Number: NASA-CR-118322
Accession Number
71N25237
Funding Number(s)
CONTRACT_GRANT: NAS5-21080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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