Published January 1, 1991 | Version v1
Journal article

Lunar mission design using nuclear thermal rockets

  • 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--.