The design and development of the electrical power subsystem for the lunar module are discussed. The initial requirements, the concepts used to design the subsystem, and the testing program are explained. Specific problems and the modifications or compromises (or both) imposed for resolution are detailed. The flight performance of the subsystem is described, and recommendations pertaining to power specifications for future space applications are made. (Author)
APOLLO Experience Report Lunar Module Electrical Power Subsystem
1972
17 pages
Report
Keine Angabe
Englisch