Published 1985
| Version v1
Book
Rotary radiators for reduced space powerplant temperatures
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