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Apollo 14 command module Kitty Hawk at Kennedy Space Center, Florida. Apollo 15 command module Endeavour at the National Museum of the United States Air Force, Dayton, Ohio. Crew: 3; Crew cabin volume: 210 cu ft (5.9 m 3) living space, pressurized 366 cu ft (10.4 m 3) Length: 11.4 ft (3.5 m) Diameter: 12.8 ft (3.9 m) Mass: 12,250 lb (5,560 kg)
Apollo Command Module and its position on top of Saturn V. ... The main solid-fuel rocket motor inside a long tube, with four exhaust nozzles mounted under a conical ...
Command module Columbia (CM-107) is the spacecraft that served as the command module during Apollo 11, which was the first mission to land humans on the Moon. Columbia is the only spacecraft of the 1969 Apollo 11 mission that returned to Earth .
Apollo 13 was slated to be the third landing on the moon after Apollo 8 (1968) and Apollo 12 (1969). Launched on April 11, 1970, the crew was led by commander Lovell, along with command module ...
The Apollo Guidance Computer (AGC) was a digital computer produced for the Apollo program that was installed on board each Apollo command module (CM) and Apollo Lunar Module (LM). The AGC provided computation and electronic interfaces for guidance, navigation, and control of the spacecraft. [ 3 ]
Apollo 1, initially designated AS-204, was planned to be the first crewed mission of the Apollo program, [1] the American undertaking to land the first man on the Moon. It was planned to launch on February 21, 1967, as the first low Earth orbital test of the Apollo command and service module.
The Apollo Command Module reentered with the center of mass offset from the center line; this caused the capsule to assume an angled attitude through the air, providing a sideways lift to be used for directional control. Rotational thrusters were used to steer the capsule under either automatic or manual control by changing the lift vector.
Apollo Command Module primary guidance system components Apollo Lunar Module primary guidance system components Apollo Inertial Measurement Unit. The Apollo primary guidance, navigation, and control system (PGNCS, pronounced pings) was a self-contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either as ...