The Apollo command and service module (CSM) was one of two principal components of the United States Apollo spacecraft, used for the Apollo program, which landed astronauts on the …

Propulsion Systems Overview • Define the systems for CSM propulsion and control

Apollo 16 – Small burn holes caused by yaw engine firings 3⁄4 Tests determined maximum pressure and planned for on-the-water operation of the system if required Lesson Objectives …

Component Certification and Qualification of the CSM RCS qualification test program was conducted for each component in the CSM RCS. These tests included a demonstration of the …

Spacecraft: Apollo CSM, CSM RCS. MSC approved North American's concept for thermal control of the valves in the CM's reaction control system (essential for long-duration missions).

The Apollo command service module includes two separate reaction control systems completely independent designated SM RCS and CM RCS. The SM RCS is utilized to control S/C rates …

The Reaction Control System (RCS) provides the thrust to control spacecraft rates and rotation in all three axis in addition to any minor translation maneuvers. The CSM includes two separate …

2016年2月29日 · The Apollo 13 crew commented on the difficulty of maneuvering the joined ship using only the LM's thrusters; presumably the CSM RCS was entirely shut down at that point, …

Spacecraft: Apollo LM, CSM Block I, LM RCS. MSC established the configuration of the reaction control system engines for both the service module (SM) and the LEM, and informed North …

The forward compartment held two reaction control system (RCS) engines, three landing parachutes and two drogue parachutes. When the CM returned from space, the heat shield …