Published 1989
| Version v1
Report
Restricted
Safety testing program for the Galileo mission radioisotope thermoelectric generator
Description
The major design requirement for any space nuclear power system is to minimize the potential for interaction of the radioactive materials with Earth's population and environment. All previous space power systems were launched on expendable launch vehicles (ELVs), so the design emphasis for the GPHS was on surviving the most severe ELV accident environments (launch pad explosion and solid propellant fire) and on surviving accident environments resulting from spacecraft failure (reentry and land impact). 14 refs., 4 figs., 2 tabs
Availability note (English)
MF available from INIS under the Report Number; Available from NTIS, PC A03/MF A01 - OSTI; 1 as DE89011192.
Files
Additional details
Publishing Information
- Imprint Pagination
- 16 p.
- Report number
- LA-UR--89-1178
Conference
- Title
- 9. international system safety conference.
- Dates
- 17-20 Jul 1989.
- Place
- Long Beach, CA (USA).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 20068651
- Subject category
- S61: RADIATION PROTECTION AND DOSIMETRY;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- ACCIDENTS; FIRES; IMPACT TESTS; RADIOISOTOPE GENERATORS; RADIOISOTOPE HEAT SOURCES; REACTOR SAFETY; REENTRY; SAFETY ENGINEERING; SPACE VEHICLES; SPACECRAFT POWER SUPPLIES
- Descriptors DEC
- ELECTRONIC EQUIPMENT; ENERGY SOURCES; EQUIPMENT; MATERIALS TESTING; MECHANICAL TESTS; POWER SUPPLIES; SAFETY; TESTING
Optional Information
- Notes
- Portions of this document are illegible in microfiche products.
- Secondary number(s)
- CONF-890780--1.