The duty cycle for the LM-11 APS consisted of two firings, an ascent stage liftoff from the lunar surface, and the terminal phase initiation (TPI) burn. APS performance for the first firing was evaluated and found to be satisfactory. No propulsion data were received from the second APS burn; however, all indications were that the burn was nominal. Engine ignition for the APS lunar liftoff burn occured at the Apollo elapsed time (AET) of 175:31:47.9 (hours:minutes:seconds). Burn duration was 427.7 seconds
This report describes the process of crew procedures development used in the Apollo Program. The two...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the lunar module landing gear subsystem through the Apollo 11 lunar landing missi...
Results from the postflight analysis of the ascent propulsion system (APS) performance during the Ap...
The performance of the LM-11 descent propulsion system during the Apollo 16 missions was evaluated a...
Steady state performance analysis for ascent propulsion system during Apollo 9 mission burn to deple...
The Apollo 16 Mission was the sixteenth in a series of flights using Apollo flight hardware and incl...
Activities involved in the performance analysis of the Apollo lunar module ascent propulsion system ...
The results are presented of the postflight analysis of the ascent propulsion system (APS) performan...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The command and service module 112 service propulsion system performance for the Apollo 15 mission w...
The design, development and qualification of the reaction control system for the Apollo lunar module...
Evaluation of flight performance of service propulsion system during Apollo 8 Missio
Spacecraft velocity data and crew reports indicated that RCS engine performance was nominal. It is e...
A postflight analysis of the Apollo 14 flight is presented. The basic objective of the flight evalua...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the lunar module landing gear subsystem through the Apollo 11 lunar landing missi...
Results from the postflight analysis of the ascent propulsion system (APS) performance during the Ap...
The performance of the LM-11 descent propulsion system during the Apollo 16 missions was evaluated a...
Steady state performance analysis for ascent propulsion system during Apollo 9 mission burn to deple...
The Apollo 16 Mission was the sixteenth in a series of flights using Apollo flight hardware and incl...
Activities involved in the performance analysis of the Apollo lunar module ascent propulsion system ...
The results are presented of the postflight analysis of the ascent propulsion system (APS) performan...
The development of the Apollo lunar module ascent propulsion subsystem is documented. The ascent pro...
The command and service module 112 service propulsion system performance for the Apollo 15 mission w...
The design, development and qualification of the reaction control system for the Apollo lunar module...
Evaluation of flight performance of service propulsion system during Apollo 8 Missio
Spacecraft velocity data and crew reports indicated that RCS engine performance was nominal. It is e...
A postflight analysis of the Apollo 14 flight is presented. The basic objective of the flight evalua...
This report describes the process of crew procedures development used in the Apollo Program. The two...
The significant service propulsion subsystem development, qualification, and flight experience from ...
The development of the lunar module landing gear subsystem through the Apollo 11 lunar landing missi...