Apollo

The Apollo spacecraft was composed of three parts designed to accomplish the American Apollo program's goal of landing astronauts on the Moon by the end of the 1960s and returning them safely to Earth. The expendable (single-use) spacecraft consisted of a combined command and service module (CSM) and an Apollo Lunar Module (LM). Two additional components complemented the spacecraft stack for space vehicle assembly: a spacecraft–LM adapter (SLA) designed to shield the LM from the aerodynamic stress of launch and to connect the CSM to the Saturn launch vehicle and a launch escape system (LES) to carry the crew in the command module safely away from the launch vehicle in the event of a launch emergency.

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Frameless

Command Module diagram

Apollo CSM lunar orbit

Apollo 17 Command Module AS17-145-22261HR

ISS053-E-419836 - View of Earth

Type	Subtype	Date	Description	Notes	Source
commons	image		Command Module diagram		Commons
commons	image		Apollo CSM lunar orbit		Commons
commons	image		Apollo 17 Command Module AS17-145-22261HR		Commons
commons	image		ISS053-E-419836 - View of Earth		Commons