Actions for Light-weight radioisotope heater impact tests [electronic resource].
Light-weight radioisotope heater impact tests [electronic resource].
- Published
- Washington, D.C. : United States. Dept. of Energy, 1998.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy. - Physical Description
- 9 pages : digital, PDF file
- Additional Creators
- Los Alamos National Laboratory, United States. Department of Energy, and United States. Department of Energy. Office of Scientific and Technical Information
Access Online
- Restrictions on Access
- Free-to-read Unrestricted online access
- Summary
- The light-weight radioisotope heater unit (LWRHU) is a ²³⁸PuO₂-fueled heat source designed to provide one thermal watt in each of various locations on a spacecraft. Los Alamos National Laboratory designed, fabricated, and safety tested the LWRHU. The heat source consists of a hot-pressed ²³⁸PuO₂ fuel pellet, a Pt-30Rh vented capsule, a pyrolytic graphite insulator, and a fineweave-pierced fabric graphite aeroshell assembly. To compare the performance of the LWRHUs fabricated for the Cassini mission with the performance of those fabricated for the Galileo mission, and to determine a failure threshold, two types of impact tests were conducted. A post-reentry impact test was performed on one of 180 flight-quality units produced for the Cassini mission and a series of sequential impact tests using simulant-fueled LWRHU capsules were conducted respectively. The results showed that deformation and fuel containment of the impacted Cassini LWRHU was similar to that of a previously tested Galileo LWRHU. Both units sustained minimal deformation of the aeroshell and fueled capsule; the fuel was entirely contained by the platinum capsule. Sequential impacting, in both end-on and side-on orientations, resulted in increased damage with each subsequent impact. Sequential impacting of the LWRHU appears to result in slightly greater damage than a single impact at the final impact velocity of 50 m/s.
- Report Numbers
- E 1.99:la-ur--97-3390
E 1.99: conf-980103--
conf-980103--
la-ur--97-3390 - Subject(s)
- Other Subject(s)
- Note
- Published through SciTech Connect.
12/31/1998.
"la-ur--97-3390"
" conf-980103--"
"DE98001474"
Space technology and applications international forum, Albuquerque, NM (United States), 25-29 Jan 1998.
Rinehart, G.H.; Herrera, A.; Reimus, M.A.H. - Funding Information
- W-7405-ENG-36
View MARC record | catkey: 14403721