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Title: Thermion: Verification of a thermionic heat pipe in microgravity. Final Report, 1990 - 1991

Technical Report ·
OSTI ID:7239615

The design and development is examined of a small excore heat pipe thermionic space nuclear reactor power system (SEHPTR). The need was identified for an in-space flight demonstration of a solar powered, thermionic heat pipe element. A demonstration would examine its performance and verify its operation in microgravity. The design of a microsatellite based technology demonstration experiment is proposed to measure the effects of microgravity on the performance of an integrated thermionic heat pipe device in low earth orbit. The specific objectives are to verify the operation of the liquid metal heat pipe and the cesium reservior in the space environment. Two design configurations are described; THERMION-I and THERMION-II. THERMION-I is designed for a long lifetime study of the operations of the thermionic heat pipe element in low earth orbit. Heat input to the element is furnished by a large mirror which collects solar energy and focuses it into a cavity containing the heat pipe device. THERMION-II is a much simpler device which is used for short term operation. This experiment remains attached to the Delta II second stage and uses energy from 500 lb of alkaline batteries to supply heat energy to the heat pipe device.

Research Organization:
Utah State Univ., Logan, UT (United States)
OSTI ID:
7239615
Report Number(s):
N-92-24794; NASA-CR-190010; NAS-1.26:190010; CNN: NASW-4435
Resource Relation:
Other Information: Original contains color illustrations
Country of Publication:
United States
Language:
English