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Title: Rotating solid radiative coolant system for space nuclear reactors

Conference ·
OSTI ID:7100351

The RING power system described in this paper is proposed as a primary or emergency heat rejection system for advanced space reactor power applications. The system employs a set of four (4) counter-rotating, 90 degree offset, coolant-carrying rings. The rings (segmented, corrugated, finned, thin-walled pipes, filled with liquid lithium) pass through a cavity heat exchanger and reradiate the absorbed heat to the space environment. 25 refs., 6 figs., 3 tabs.

Research Organization:
Pacific Northwest Lab., Richland, WA (USA)
DOE Contract Number:
AC06-76RL01830
OSTI ID:
7100351
Report Number(s):
PNL-SA-15433; CONF-880764-4; ON: DE88016312
Resource Relation:
Conference: 24. AIAA/ASME/SAE/ASEE joint propulsion conference, Boston, MA, USA, 11 Jul 1988; Other Information: Portions of this document are illegible in microfiche products
Country of Publication:
United States
Language:
English