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“阿波罗”宇宙飞船的三个舱体;指挥舱（CM）,服务舱（SM）和登月舱（LM）,每一舱体都具有自己的喷气控制系统（RCS）。每个喷气控制系统工作在自燃的双组元燃料,而燃料的供给是挤压式。 服务舱的喷气控制系统是用于在宇宙飞船与运载火箭——土星——V号分离后,在飞向月球的轨道上来控制飞船的姿态,以及在绕月球的等候轨道和返回地球轨道上来控制指挥舱和服务舱。登月舱的喷气控制系统是用于在绕地球的等候轨道上,来调整宇宙飞船与登月舱的连接形态,以及在下降到月面时和从月面起飞后与指挥服务舱交会对接时来控制登月舱。指挥舱的喷气控制系统是用于在再入大气层后,来控制指挥舱的姿态。登月舱和服务舱的喷气控制系统应能提供在三个轴方向上的位移,并同时在定向的控制状态中工作,而指挥舱的喷气控制系统仅用于定向的控制。
Three capsules of the Apollo spacecraft; CM, SM and LM, each with their own Jet Control System (RCS). Each jet control system operates on a self-igniting bipropellant while the fuel supply is squeezed. The service cockpit control system is used to control the attitude of the spacecraft after it has been separated from the launch vehicle Saturn-V from orbiting the moon, as well as on the orbit around the moon and the return to Earth orbit Command and service modules. The lunar module’s jet control system is used to adjust the connection between the spacecraft and the lunar module on a waiting orbit around the Earth and to interface with the command service capsule when descending to the lunar surface and after taking off from the lunar surface To control the lunar module. The command cabin jet control system is used to control the attitude of the command module after reentry into the atmosphere. The jet control system in the lunar module and service module should be able to provide displacement in three axes and at the same time work in directional control while the jet control system in the command module should only be used for directional control.