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  2. Apollo Guidance Computer - Wikipedia

    en.wikipedia.org/wiki/Apollo_Guidance_Computer

    The Apollo flight computer was the first computer to use silicon IC chips. [15] While the Block I version used 4,100 ICs, each containing a single three-input NOR gate, the later Block II version (used in the crewed flights) used about 2,800 ICs, mostly dual three-input NOR gates and smaller numbers of expanders and sense amplifiers.

  3. Electric gate - Wikipedia

    en.wikipedia.org/wiki/Electric_gate

    To conform to these regulations the gate system must be checked with a calibrated force tester and the full results kept in a technical file for 7 years. If the gate is not tested it does not comply. Most gate kits can be fitted with safety equipment so that these limits are achieved and so cover that part of EN13241-1.

  4. Apollo command and service module - Wikipedia

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

    Block II incorporated a revised CM heat shield design, which was tested on the uncrewed Apollo 4 and Apollo 6 flights, so the first all-up Block II spacecraft flew on the first crewed mission, Apollo 7. The two blocks were essentially similar in overall dimensions, but several design improvements resulted in weight reduction in Block II.

  5. Galileo GDS - Wikipedia

    en.wikipedia.org/wiki/Galileo_GDS

    The system was originally known as Apollo, launched in 1971 by United Airlines as their in-house booking system. In 1976, UA began installing Apollo terminals in travel agent offices. Apollo, and the competing American Airlines system Sabre , quickly took over much of the booking market.

  6. Apollo VP3 - Wikipedia

    en.wikipedia.org/wiki/Apollo_VP3

    On its time Apollo VP3 was a high performance, cost effective, and energy efficient chipset. It offered AGP support for Socket 7 processors which was not supported at that moment by Intel, SiS and ALi chipsets. In November 1997 FIC released motherboard PA-2012, which uses Apollo VP3 and has AGP bus. This was the first Socket 7 motherboard ...

  7. Ascent propulsion system - Wikipedia

    en.wikipedia.org/wiki/Ascent_Propulsion_System

    The engine developed about 1,600 pounds-force (7.1 kN) of thrust, which produced a velocity of 3,200 meters per second from lunar launch, to LOR, and CM docking. [ 7 ] [ 2 ] Lunar ascent by Apollo 17 ascent stage.

  8. Apollo abort modes - Wikipedia

    en.wikipedia.org/wiki/Apollo_abort_modes

    Apollo Launch Escape System diagram. If the rocket failed in the last five minutes before launch, the CM and the launch escape system (LES, see figure) would separate from the remainder of the rocket below with the LES propelling itself and the CM beneath it upward and eastward to the sea using a small solid-fueled motor (the launch escape motor) at the top of the tower on the launch escape ...

  9. List of Apollo missions - Wikipedia

    en.wikipedia.org/wiki/List_of_Apollo_missions

    This crewed flight was to have followed the first three uncrewed flights. After the fire which killed the AS-204 crew on the pad during a test and training exercise, uncrewed Apollo flights resumed to test the Saturn V launch vehicle and the Lunar Module; these were designated Apollo 4, 5 and 6. The first crewed Apollo mission was thus Apollo 7 ...