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

Restricted

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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.