To transfer the waste heat from a next generation spacecraft into the space the now used liquid pumping systems can be changed by capillary driven heat pipe systems which are not so unreliable considering the micrometeoroid puncture. The two phase space radiator working with amonia was tested under vacuum and temperatures about 0 Cel. The automation aspects of assembling, monitoring and controlling of the space radiator systems, the wreckage conditions, and next technology steps are discussed as well as the NASA's procedures and approach by starting this effort. (Jarc)
Space station thermal control
Die thermische Ueberwachung des Raumfahrzeuges
Mechanical Engineering ; 106 , 12 ; 22-33
1984
12 Seiten, 17 Bilder
Article (Journal)
English
Space station ECLSS and thermal control : papers
TIBKAT | 1991
|Space station active thermal control system modelling
Tema Archive | 1987
|Space-station active thermal control system modeling
Tema Archive | 1988
|