Add to ORKGThe reaction control systems of the Apollo command and service module were developed and modified be...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...
The Apollo launch escape propulsion subsystem contained three solid rocket motors. The general desig...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
Simulated space environment performance tests of Apollo lunar module in thermal vacuum environmen
Qualifications tests on applications technology satellite apogee rocket motor assemblie
The design, development and qualification of the reaction control system for the Apollo lunar module...
Wind tunnel investigation of aerodynamic pressures on Apollo launch escape vehicle configuratio
Environmental acceptance testing was used extensively to screen selected spacecraft hardware for wor...
A review of the Apollo spacecraft certification (qualification) test program is presented. The appro...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
The duty cycle for the LM-11 APS consisted of two firings, an ascent stage liftoff from the lunar su...
Aerodynamic characteristics determined during development of Apollo launch escape vehicle configurat...
Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsio...
The reaction control systems of the Apollo command and service module were developed and modified be...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...
The Apollo launch escape propulsion subsystem contained three solid rocket motors. The general desig...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
Simulated space environment performance tests of Apollo lunar module in thermal vacuum environmen
Qualifications tests on applications technology satellite apogee rocket motor assemblie
The design, development and qualification of the reaction control system for the Apollo lunar module...
Wind tunnel investigation of aerodynamic pressures on Apollo launch escape vehicle configuratio
Environmental acceptance testing was used extensively to screen selected spacecraft hardware for wor...
A review of the Apollo spacecraft certification (qualification) test program is presented. The appro...
Development flight instrumentation was delivered for 25 Apollo vehicles as Government-furnished equi...
The duty cycle for the LM-11 APS consisted of two firings, an ascent stage liftoff from the lunar su...
Aerodynamic characteristics determined during development of Apollo launch escape vehicle configurat...
Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsio...
The reaction control systems of the Apollo command and service module were developed and modified be...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
Portions of the combined Apollo spacecraft (the command and service module and the lunar module) are...