Orbit to surface beamed power for Mars bases expansion
Creators
- 1. National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
Description
A scenario is presented wherein the interplanetary supply vehicles for the expansion of the Mars bases are nuclear powered-electrically propelled. For the initial build-up phase every supply vehicle need not return to earth but could be utilized as a one-way transport to Mars synchronous orbit. Upon arriving at Mars., they would land their cargos with one-way descent vehicles. Base personnel will arrive at Mars in separate 'fast trip' vehicles. Once in the Mars synchronous orbits, the nuclear power system is will longer be needed for propulsion. Thus, this power system - megawatt power range - can be used as an orbital power station beaming its power to locations on the surface of the planet. Placing a number of such power systems at strategically located synchronous orbit positions will permit coverage of the major portion of the Martian surface. The megawatt size power system for one interplanetary electric propulsion vehicle will be capable of supplying a number of surface bases of installations
Additional details
Publishing Information
- Publisher
- IEEE Service Center.
- Imprint Place
- Piscataway, NJ (USA)
- Imprint Title
- Proceedings of the 24th intersociety energy conversion engineering conference. Volume 1
- Imprint Pagination
- 2950 p.
- Series
- Aerospace power systems and power conditioning.
- Journal Page Range
- p. 479-484.
Conference
- Title
- 24. intersociety energy conversion engineering conference.
- Dates
- 6-11 Aug 1989.
- Place
- Arlington, VA (USA).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 21036927
- Subject category
- S21: SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- MARS SPACE PROBES; SPACE FLIGHT; SPACE POWER REACTORS
- Descriptors DEC
- MOBILE REACTORS; POWER REACTORS; REACTORS; SPACE VEHICLES
Optional Information
- Notes
- Imprint:Technical Paper 899139.
- Secondary number(s)
- CONF-890815--.