Lunar mission design using nuclear thermal rockets
Creators
- 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)
Description
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
Additional details
Publishing Information
- Journal Title
- AIP Conference Proceedings
- Journal Volume
- 217
- Journal Issue
- 1
- Series
- AIP Conf. Proc.
- Journal Page Range
- 100-105
- ISSN
- 0094-243X
- CODEN
- APCPC
Conference
- Title
- 8. symposium on space nuclear power systems.
- Dates
- 6-10 Jan 1991.
- Place
- Albuquerque, NM (USA).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 22077235
- Subject category
- S42: ENGINEERING; S21: SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- MARS SPACE PROBES; MOON; ORBIT STABILITY; REACTOR TECHNOLOGY; ROCKETS; SPACE FLIGHT; SPACE PROPULSION REACTORS; SPACE VEHICLES; TRANSPORT
- Descriptors DEC
- MOBILE REACTORS; POWER REACTORS; PROPULSION REACTORS; REACTORS; SATELLITES; SPACE POWER REACTORS; STABILITY
Optional Information
- Secondary number(s)
- CONF-910116--.