Study of heat rejection systems
Abstract
The technology demonstration model (TDM) design developed for the Spacelab radiator heat rejection system is described. A pumped fluid loop radiator using Freon R21 as coolant is used. The following aspects of the design are included: thermal; hydraulic; structural; manufacturing process system control and performance; system tests; and component selection.
- Publication:
-
Final Report Aeritalia S.p.A
- Pub Date:
- July 1980
- Bibcode:
- 1980aers.rept.....B
- Keywords:
-
- Design Analysis;
- Spacecraft Radiators;
- Spacelab;
- Systems Engineering;
- Coolants;
- European Space Programs;
- Freon;
- Loops;
- Radiative Heat Transfer;
- Fluid Mechanics and Heat Transfer