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Low power dc arcjet operation with hydrogen/nitrogen/ammonia mixturesThe effect of gas composition and ambient pressure on arcjet operation was determined. Arcjet operation in different facilities was also compared to determine the validity of tests in small facilities. Volt-ampere characteristics were determined for an arcjet using hydrogen/nitrogen mixtures (simulating both ammonia and hydrazine), hydrogen/nitrogen/ammonia mixtures, and pure ammonia as propellants at various flow rates. The arcjet had a typical performance of 450 sec specific impulse at 1 kW with hydrogen/nitrogen mixtures. It was determined that the amount of ammonia present in the gas stream had a significant effect on the arcjet volt-ampere characteristics. Also, hydrogen/nitrogen mixtures simulating ammonia gave arc characteristics approximately the same as those of pure ammonia. Finally, no differences in arc volt-ampere characteristics were seen between low and high ambient pressure operation in the same facility. A 3 to 5 V difference was seen when different facilities were compared, but this difference was probably due to differences in the voltage drops across the current connections, and not due to arcjet operational differences in the two facilities.
Document ID
19870061301
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hardy, Terry L.
(NASA Lewis Research Center Cleveland, OH, United States)
Curran, Francis M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 87-1948
Accession Number
87A48575
Distribution Limits
Public
Copyright
Other

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