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  2. Apollo PGNCS - Wikipedia

    en.wikipedia.org/wiki/Apollo_PGNCS

    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 ...

  3. ST-124-M3 inertial platform - Wikipedia

    en.wikipedia.org/wiki/ST-124-M3_inertial_platform

    The ST-124-M3 inertial platform was a device for measuring acceleration and attitude of the Saturn V launch vehicle. It was carried by the Saturn V Instrument Unit , a 3-foot-high (0.91 m), 22-foot-diameter (6.7 m) section of the Saturn V that fit between the third stage (S-IVB) and the Apollo spacecraft.

  4. Saturn V instrument unit - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_Instrument_Unit

    IBM. "Instrument Unit System Description and Component Data." This lists, in Table 1, all components by name, part number, reference designation and location for IU-201 to -212 and IU-501 to -515. It also includes photos of many components. The change history page lists six changes, the latest being January 1970, the year IU-508 was launched.

  5. Lunar Traverse Gravimeter - Wikipedia

    en.wikipedia.org/wiki/Lunar_Traverse_Gravimeter

    Inertial guidance accelerometers, like those in intercontinental ballistic missiles, were particularly suited to the purpose of an astronaut operated traversal gravimeter due to three main attributes: a large range of sensitivity, comparatively small size and weight, and the ability to calibrate the instrument under low acceleration conditions.

  6. List of NASA's flight control positions - Wikipedia

    en.wikipedia.org/wiki/List_of_NASA's_flight...

    NASA currently has a group of flight controllers at the Johnson Space Center in Houston for the International Space Station (ISS). The Space Shuttle flight control team (as well as those for the earlier Gemini, Apollo, and Skylab programs) were also based there.

  7. J002E3 - Wikipedia

    en.wikipedia.org/wiki/J002E3

    The Apollo 12 empty S-IVB, Instrument Unit, and spacecraft adapter base, had a mass of about 14 tonnes; 15 short tons (30,000 lb). [6] This is less than one-fifth of the 77.1-tonne; 85.0-short-ton (169,900 lb) mass of the Skylab space station , which was constructed from a similar S-IVB and fell out of orbit on 11 July 1979. [ 7 ]

  8. List of astronomical instruments - Wikipedia

    en.wikipedia.org/wiki/List_of_astronomical...

    An astronomical instrument is a device for observing, measuring or recording astronomical data. They are used in the scientific field of astronomy , a natural science that studies celestial objects and the phenomena that occur in the cosmos, with the object of explaining their origin and evolution over time.

  9. Saturn V dynamic test vehicle - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_Dynamic_Test_Vehicle

    A boilerplate Apollo spacecraft, BP-27 together with LTA-2, was used for all configurations of dynamic testing. [4] [24] [25] The boilerplate took the place of actual flight hardware. Boilerplate size, shape, mass and center of gravity were the same, but it was not necessary for the entire Apollo spacecraft to be complete to commence dynamic ...