Published March 1996 | Version v1
Journal article

Fabrication of light weight radioisotope heater unit hardware components

Creators

  • 1. EG ampersand G Mound Applied Technologies, P.O. Box 3000, Miamisburg, Ohio 45343-3000 (United States)

Description

The Light Weight Radioisotope Heater Unit (LWRHU) is planned to be used on the National Aeronautics and Space Administration (NASA) Cassini Mission, to provide localized thermal energy as strategic locations on the spacecraft. These one watt heater units will support the operation of many on-board instruments that require a specific temperature range to function properly. The system incorporates a fuel pellet encapsulated in a vented metallic clad fabricated from platinum-30% rhodium (Pt-30%Rh) tubing, sheet and foil materials. To complete the package, the clad assemblies are placed inside a combination of graphite components. This report describes the techniques employed by Mound related to the fabrication and sub assembly processes of the LWRHU clad hardware components. Included are details concerning configuration control systems, material procurement and certification, hardware fabrication specifics, and special processes that are utilized. copyright 1996 American Institute of Physics

Additional details

Publishing Information

Journal Title
AIP Conference Proceedings
Journal Volume
361
Journal Issue
1
Journal Page Range
p. 1043-1048.
ISSN
0094-243X
CODEN
APCPCS

Conference

Title
space technology and applications international forum.
Acronym
STAIF 96
Dates
7-11 Jan 1996.
Place
Albuquerque, NM (United States).

Optional Information

Secondary number(s)
CONF-960109--.