Published 1989 | Version v1
Book

Orbit to surface beamed power for Mars bases expansion

  • 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--.