Add to ORKGExperience with the Apollo command service module and lunar module batteries is discussed. Significant hardware development concepts and hardware test results are summarized, and the operational performance of batteries on the Apollo 7 to 13 missions is discussed in terms of performance data, mission constraints, and basic hardware design and capability. Also, the flight performance of the Apollo battery charger is discussed. Inflight data are presented
A review of the concept, operational requirements, design, and development of the lunar module missi...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
A developmental history of the Apollo lunar module landing and rendezvous radar subsystems is presen...
The design and development of the electrical power subsystem for the lunar module are discussed. The...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The design concepts and philosophies of the lunar module instrumentation subsystem are discussed alo...
Objectives include: a) Describe LM Electrical System original specifications; b) Describe the decisi...
The development of the lunar module communications system is traced from the initial concept to the ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
A review of the Apollo command and service module instrumentation subsystem is presented. The measur...
The design, development and qualification of the reaction control system for the Apollo lunar module...
A comprehensive review of the design philosophy and experience of the Apollo electrical power genera...
A brief record of the development and use of the orbital-rate-drive assembly in the Apollo Program i...
The development of the lunar module landing gear subsystem through the Apollo 11 lunar landing missi...
Various phases of the postflight testing of the command modules used in the Apollo Program are prese...
A review of the concept, operational requirements, design, and development of the lunar module missi...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
A developmental history of the Apollo lunar module landing and rendezvous radar subsystems is presen...
The design and development of the electrical power subsystem for the lunar module are discussed. The...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The design concepts and philosophies of the lunar module instrumentation subsystem are discussed alo...
Objectives include: a) Describe LM Electrical System original specifications; b) Describe the decisi...
The development of the lunar module communications system is traced from the initial concept to the ...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
A review of the Apollo command and service module instrumentation subsystem is presented. The measur...
The design, development and qualification of the reaction control system for the Apollo lunar module...
A comprehensive review of the design philosophy and experience of the Apollo electrical power genera...
A brief record of the development and use of the orbital-rate-drive assembly in the Apollo Program i...
The development of the lunar module landing gear subsystem through the Apollo 11 lunar landing missi...
Various phases of the postflight testing of the command modules used in the Apollo Program are prese...
A review of the concept, operational requirements, design, and development of the lunar module missi...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
A developmental history of the Apollo lunar module landing and rendezvous radar subsystems is presen...