Phase 1 space fission propulsion system design considerations
Author(s) -
Mike Houts,
Melissa Van Dyke,
Tom Godfroy,
Kevin Pedersen,
James A. Martin,
Ricky Dickens,
Pat Salvail,
Ivana Hrbud,
Rob Carter
Publication year - 2002
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.1449776
Subject(s) - propulsion , in space propulsion technologies , schedule , electric power system , electrically powered spacecraft propulsion , computer science , testability , automotive engineering , engineering , reliability engineering , power (physics) , aerospace engineering , operating system , physics , quantum mechanics
Fission technology can enable rapid, affordable access to any point in the solar system. If fission propulsion systems are to be developed to their full potential; however, near-term customers must be identified and initial fission systems successfully developed, launched, and operated. Studies conducted in fiscal year 2001 (IISTP, 2001) show that fission electric propulsion (FEP) systems operating at 80 kWe or above could enhance or enable numerous robotic outer solar system missions of interest. At these power levels it is possible to develop safe, affordable systems that meet mission performance requirements. In selecting the system design to pursue, seven evaluation criteria were identified: safety, reliability, testability, specific mass, cost, schedule, and programmatic risk. A top-level comparison of three potential concepts was performed: an SP-100 based pumped liquid lithium system, a direct gas cooled system, and a heatpipe cooled system. For power levels up to at least 500 kWt (enabling electri...
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