The service propulsion system gimbal actuators of the Apollo command and service module were developed, modified, and qualified between February 1962 and April 1968. The development of these actuators is described as the result of extensive testing, retesting, and modification of the initial design. Successful completion of each mission without anomalies attributable to the actuators indicated that the particular configuration (modification) in use was adequate for the flight profile imposed.
Apollo experience report: Guidance and control systems: CSM service propulsion system gimbal actuators
1975-07-01
Miscellaneous
No indication
English
Apollo Experience Report: Service Propulsion Subsystem
NTIS | 1973
|Apollo experience report: Service propulsion subsystem
NTRS | 1973
|Apollo experience report ; [58]: Service propulsion subsystem
TIBKAT | 1973
|