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S-Band laboratory test equipment Final reportSubsystem component design and development, and system performance of ammonia fueled resistojet thrustor for spacecraft inversion maneuvers
Document ID
19670006349
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
John, R. R. (Avco Corp. Wilmington, MA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72123
AVSSD-0356-66-CR, SUPPL. 1
Report Number: NASA-CR-72123
Report Number: AVSSD-0356-66-CR, SUPPL. 1
Accession Number
67N15678
Funding Number(s)
CONTRACT_GRANT: NAS3-5908
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RESISTOJET ENGINE
THRUSTOR
INVERSION
ATTITUDE CONTROL
SPACECRAFT MANEUVER
ELECTROTHERMAL ENGINE

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