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Title: Galileo light-weight radioisotope heater units design and safety analysis

Conference ·
OSTI ID:6649215
 [1];  [2]
  1. EG and G Mound Applied Technologies, Miamisburg, OH (USA)
  2. Los Alamos National Lab., NM (USA)

The Light-Weight Radioisotope Heater Unit (LWRHU) provides thermal energy to temperature sensitive components aboard the orbiter/probe of the Galileo Spacecraft during its multiyear interplanetary mission. Heat is derived from the radioisotopic decay of 238-plutonium. A power of 0.56 watts/gram of radioisotope, a half-life of 88 years, and no moving parts permitted a robust, long-lived, compact heat source design. A single l-w design provided small thermal increments, with options in the number and placement, to satisfy the needed thermal environment for the spacecraft components. Radioisotope use in these devices necessitated the assessment of postulated radiological risks in accidents or malfunctions of the space shuttle or the Galileo spacecraft during near earth mission phases. Included in this document are data for the design, postulated accidents with their consequences, test data, and the derived source terms and personnel exposures for the various events. 5 refs., 1 fig., 1 tab.

Research Organization:
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States)
Sponsoring Organization:
DOE/NE
DOE Contract Number:
W-7405-ENG-36; AC04-88DP43495
OSTI ID:
6649215
Report Number(s):
LA-UR-90-2164; CONF-901101-16; ON: DE90013151
Resource Relation:
Conference: American Nuclear Society winter meeting, Washington, DC (USA), 11-15 Nov 1990
Country of Publication:
United States
Language:
English