A heatpipe experiment for a long duration exposure facility is described. The design and configuration of the power system of the spacecraft is reported with emphasis placed on its solar array panels, 12-ampere hour 18-cell nickel battery, and its electronic controller.
The LDEF heat pipe experiment power systems
01.04.1980
Aufsatz (Konferenz)
Keine Angabe
Englisch
Tema Archiv | 1978