Conceptual spacecraft and arcjet propulsion system design for the SP-100 interim reference missionAn arcjet propulsion system, delivering 7.5 N thrust, was defined for the SP-100 Space Reactor Power System Interim Reference Mission. Conceptual design trades and configuration studies of a spacecraft suitable for the mission were performed to the extent necessary to define propulsion system requirements and interfaces. The propulsion system design is based on the use of 30-kW, constricted arc, ammonia arcjet engines operating in parallel during orbit boost from low earth to geosynchronous orbit.
Document ID
19900055487
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zafran, S. (TRW, Inc. Redondo Beach, CA, United States)
Bell, M. W. J. (TRW Space and Technology Group Redondo Beach, CA, United States)