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  2. Descent propulsion system - Wikipedia

    en.wikipedia.org/wiki/Descent_propulsion_system

    Descent propulsion system. The descent propulsion system (DPS - pronounced 'dips') or lunar module descent engine (LMDE), internal designation VTR-10, is a variable- throttle hypergolic rocket engine invented by Gerard W. Elverum Jr. [3] [4] [5] and developed by Space Technology Laboratories (TRW) for use in the Apollo Lunar Module descent stage.

  3. Ascent propulsion system - Wikipedia

    en.wikipedia.org/wiki/Ascent_Propulsion_System

    The ascent propulsion system ( APS) or lunar module ascent engine ( LMAE) is a fixed- thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module ascent stage. It used Aerozine 50 fuel, and N. 4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion ...

  4. Apollo command and service module - Wikipedia

    en.wikipedia.org/wiki/Apollo_command_and_service...

    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 Moon between 1969 and 1972. The CSM functioned as a mother ship, which carried a crew of three astronauts and the second Apollo spacecraft, the Apollo Lunar Module ...

  5. Apollo TV camera - Wikipedia

    en.wikipedia.org/wiki/Apollo_TV_camera

    The camera was stowed in the LM, and it used the LM's communications systems to evaluate their performance before lunar operations began. This meant that the CM did not carry a video camera for this mission. It was next used on Apollo 11, carried in the LM's descent stage, in the quad 4 Modularized Equipment Stowage Assembly (MESA).

  6. Tiangong space station - Wikipedia

    en.wikipedia.org/wiki/Tiangong_space_station

    The module is divided into multiple sections, including the pressurised crew working compartment, the unpressurised cargo section, the cargo airlock/on-orbit release mechanism, as well as the control module section featuring external experiment adapters, a communication antenna, and two solar arrays.

  7. Apollo Guidance Computer - Wikipedia

    en.wikipedia.org/wiki/Apollo_Guidance_Computer

    Dimensions. 24 in × 12.5 in × 6.5 in (61 cm × 32 cm × 17 cm) 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 ...

  8. LM317 - Wikipedia

    en.wikipedia.org/wiki/LM317

    LM317 with heat sink. The LM317 is an adjustable positive linear voltage regulator. It was designed by Bob Dobkin in 1976 while he worked at National Semiconductor. [1] The LM337 is the negative complement to the LM317, which regulates voltages below a reference. It was designed by Bob Pease, who also worked for National Semiconductor.

  9. General Electric LM2500 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_LM2500

    First run. 1960s. Developed from. General Electric CF6. The General Electric LM2500 is an industrial and marine gas turbine produced by GE Aviation. The LM2500 is a derivative of the General Electric CF6 aircraft engine. As of 2004, the U.S. Navy and at least 29 other navies had used a total of more than one thousand LM2500/LM2500+ gas turbines ...

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