Four advanced space radiator concepts that were pursued in an integrated effort to develop multi-mission-use and low cost heat rejection systems which can overcome the limitations of current radiator systems are briefly discussed and described. Also, in order to establish a firm background to compare the advanced space radiator concepts, the Orbiter active thermal control system is also briefly described.
Spacecraft active thermal control technology status
01.09.1978
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTRS | 1973