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Nuclear propulsion tradeoffs for manned Mars missions

Conference · · AIP Conference Proceedings (American Institute of Physics); (United States)
DOI:https://doi.org/10.1063/1.40112· OSTI ID:5484636
;  [1]
  1. B W Nuclear Technologies, Space Defense Systems, P.O. Box 10935, Lynchburg, Virginia 24506-0935 (US)
A conjunction class split/sprint manned Mars exploration mission was studied to evaluate tradeoffs in performance characteristics of nuclear thermal rockets. A Particle Bed Reactor-based nuclear thermal rocket was found to offer a 38% to 52% total mass savings compared with a NERVA-based nuclear thermal rocket for this mission. This advantage is primarily due to the higher thrust-to-weight ratio of the Particle Bed Reactor nuclear rocket. The mission is enabled by nuclear thermal rockets. It cannot be performed practically using chemical propulsion.
OSTI ID:
5484636
Report Number(s):
CONF-910116--
Conference Information:
Journal Name: AIP Conference Proceedings (American Institute of Physics); (United States) Journal Volume: 217:2
Country of Publication:
United States
Language:
English