Space Station Freedom thermal control and life support system design

Abstract

The Space Station Freedom thermal control system (TCS) and environmental control and life support system (ECLSS) are reviewed. Differences in the TCS and ECLSS are discussed between the early man-tended configuration (MTC) compared to the eventual evolutions to the permanently manned configuration (PMC). Concurrent analytical and developmental testing programs are included in the systems discussions as well as a description of an early 1993 flight test program on elements of the PMC water recovery system. Recent TCS design changes to the air cooling of rack mounted equipment are discussed. An overview of all TCS and ECLSS subsystems is included.