Published 1985 | Version v1
Book

Rotary radiators for reduced space powerplant temperatures

Creators

  • 1. Jet Propulsion Lab., Pasadena, CA

Description

If new radiator concepts can achieve radiator weights below 3 kg/m2, nuclear space powerplants can operate at temperatures below 9000K and use stainless steel construction. Tube-and-fin or heat-pipe radiators weight at least 5 kg/m2 because the tube walls must be thick enough to prevent or limit meteoroid punctures. However, radiators that require no meteoroid protection can be built using low-vapor-pressure liquids that can be exposed directly to space. One possible design for such a radiator is the ''rotary radiator'' that uses centrifugal force to move the liquid across a thin radiating disk and uses surface tension to retain the liquid despite meteoroid punctures. 12 refs., 11 figs

Additional details

Publishing Information

Publisher
Orbit Book Company, Inc.
Imprint Place
Malabar, FL (USA)
Imprint Title
Space nuclear power systems 1984: proceedings. Volume 2
Journal Page Range
p. 447-453.

Conference

Title
Symposium on space nuclear power systems.
Dates
10-13 Jan 1984.
Place
Albuquerque, NM (USA).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
18083305
Subject category
S21: SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS; S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
BRAYTON CYCLE; HEAT TRANSFER; HYDRAULICS; RADIATORS; RANKINE CYCLE; SPACE POWER REACTORS; SPECIFICATIONS; WEIGHT
Descriptors DEC
ENERGY TRANSFER; HEAT EXCHANGERS; MOBILE REACTORS; POWER REACTORS; REACTORS; THERMODYNAMIC CYCLES