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Title: Lunar mission design using nuclear thermal rockets

Conference · · AIP Conference Proceedings (American Institute of Physics); (United States)
DOI:https://doi.org/10.1063/1.40033· OSTI ID:5666297
;  [1];  [2]
  1. Science Applications International Corporation, 1515 Woodfield Road, Suite 350, Schaumburg, Illinois 60173 (USA)
  2. NASA Lewis Research Center, M/S 501-6, 21000 Brookpark Road, Cleveland, Ohio 44135 (USA)

The NERVA-class Nuclear Thermal Rocket (NTR), with performance nearly double that of advanced chemical engines, has long been considered an enabling technology for human missions to Mars. NTR engines address the demanding trip time and payload delivery needs of both cargo-only and piloted flights. But NTR can also reduce the Earth launch requirements for manned lunar missions. First use of NTR for the Moon would be less demanding and would provide a test-bed for early operations experience with this powerful technology. Study of application and design options indicates that NTR propulsion can be integrated with the Space Exploration Initiative scenarios to deliver performance gains while managing controlled, long-term disposal of spent reactors to highly stable orbits.

OSTI ID:
5666297
Report Number(s):
CONF-910116-; CODEN: APCPC; TRN: 91-019972
Journal Information:
AIP Conference Proceedings (American Institute of Physics); (United States), Vol. 217:1; Conference: 8. symposium on space nuclear power systems, Albuquerque, NM (United States), 6-10 Jan 1991; ISSN 0094-243X
Country of Publication:
United States
Language:
English