NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Space Fission Propulsion System Development StatusThe world's first man-made self-sustaining fission reaction was achieved in 1942. Since then fission has been used to propel submarines, generate tremendous amounts of electricity, produce medical isotopes, and provide numerous other benefits to society. Fission systems operate independently of solar proximity or orientation, and are thus well suited for deep space or planetary surface missions. In addition, the fuel for fission systems (enriched uranium) is virtually non-radioactive. The primary safety issue with fission systems is avoiding inadvertent system start. Addressing this issue through proper system design is straight-forward. Despite the relative simplicity and tremendous potential of space fission systems, the development and utilization of these systems has proven elusive. The first use of fission technology in space occurred 3 April 1965 with the US launch of the SNAP-10A reactor. There have been no additional US uses of space fission systems. While space fission systems were used extensively by the former Soviet Union, their application was limited to earth-orbital missions. Early space fission systems must be safely and affordably utilized if we are to reap the benefits of advanced space fission systems. NASA's Marshall Space Flight Center, working with Los Alamos National Laboratory (LANL), Sandia National Laboratories, and others, has conducted preliminary research related to a Safe Affordable Fission Engine (SAFE). An unfueled core has been fabricated by LANL, and resistance heaters used to verify predicted core thermal performance by closely mimicking heat from fission. The core is designed to use only established nuclear technology and be highly testable. In FY01 an energy conversion system and thruster will be coupled to the core, resulting in an 'end-to-end' nuclear electric propulsion demonstrator being tested using resistance heaters to closely mimic heat from fission. Results of the SAFE test program will be presented. The applicability of a SAFE-powered electric propulsion system to outer planet science missions will also be discussed.
Document ID
20010041242
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Houts, M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Van Dyke, M. K.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Godfroy, T. J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Pedersen, K. W.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Martin, J. J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Dickens, R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Williams, E.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Harper, R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Salvail, P.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Hrbud, I.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Publication Information
Publication: Forum on Innovative Approaches to Outer Planetary Exploration 2001-2020
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available