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
A safe haven and work supported PV power systems on the lunar surface will likely be required by NAS...
A trade study of power system technology for proposed lunar vehicles and servicers is presented. A v...
ABSTRACT The Power Systems branch at JSC faces a number of complex issues as it readies itself for t...
The design concepts and philosophies of the lunar module instrumentation subsystem are discussed alo...
Experience with the Apollo command service module and lunar module batteries is discussed. Significa...
A comprehensive review of the design philosophy and experience of the Apollo electrical power genera...
Objectives include: a) Describe LM Electrical System original specifications; b) Describe the decisi...
In the Apollo Program, the lunar-orbit rendezvous mode was used for the lunar-landing mission. To ac...
Design philosophies and technology needs for the power management and distribution (PMAD) portion of...
Topics concerning the Common Lunar Lander are presented in view graph form and include: energy stora...
The general requirements of the electrical wiring subsystems and the problem areas and solutions tha...
The development of the lunar module communications system is traced from the initial concept to the ...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The capacity of global power systems must be increased by a factor of ten to provide the predicted p...
A safe haven and work supported PV power systems on the lunar surface will likely be required by NAS...
A trade study of power system technology for proposed lunar vehicles and servicers is presented. A v...
ABSTRACT The Power Systems branch at JSC faces a number of complex issues as it readies itself for t...
The design concepts and philosophies of the lunar module instrumentation subsystem are discussed alo...
Experience with the Apollo command service module and lunar module batteries is discussed. Significa...
A comprehensive review of the design philosophy and experience of the Apollo electrical power genera...
Objectives include: a) Describe LM Electrical System original specifications; b) Describe the decisi...
In the Apollo Program, the lunar-orbit rendezvous mode was used for the lunar-landing mission. To ac...
Design philosophies and technology needs for the power management and distribution (PMAD) portion of...
Topics concerning the Common Lunar Lander are presented in view graph form and include: energy stora...
The general requirements of the electrical wiring subsystems and the problem areas and solutions tha...
The development of the lunar module communications system is traced from the initial concept to the ...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The capacity of global power systems must be increased by a factor of ten to provide the predicted p...
A safe haven and work supported PV power systems on the lunar surface will likely be required by NAS...
A trade study of power system technology for proposed lunar vehicles and servicers is presented. A v...
ABSTRACT The Power Systems branch at JSC faces a number of complex issues as it readies itself for t...