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Cathode studies of a radiation cooled MPD arc thrusterCathode insulator modifications of radiation cooled MPD arc thrustor tested in power range of 9.8 to 46.4 kW using ammonia as principal propellant
Document ID
19710016294
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Esker, D. W. (McDonnell-Douglas Corp. Saint Louis, MO, United States)
Kroutil, J. C. (McDonnell-Douglas Corp. Saint Louis, MO, United States)
Sedrick, A. V. (McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72891
MDC-Q0446
Report Number: NASA-CR-72891
Report Number: MDC-Q0446
Accession Number
71N25770
Funding Number(s)
CONTRACT_GRANT: NAS3-13664
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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