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  2. Space Shuttle design process - Wikipedia

    en.wikipedia.org/wiki/Space_Shuttle_design_process

    The combined space station and Air Force payload requirements were not sufficient to reach desired shuttle launch rates. Therefore, the plan was for all future U.S. space launches—space stations, Air Force, commercial satellites, and scientific research—to use only the Space Shuttle. Most other expendable boosters would be phased out.

  3. Space Shuttle - Wikipedia

    en.wikipedia.org/wiki/Space_Shuttle

    The satellite designs also required that the Space Shuttle have a 4.6 by 18 m (15 by 60 ft) payload bay. NASA evaluated the F-1 and J-2 engines from the Saturn rockets , and determined that they were insufficient for the requirements of the Space Shuttle; in July 1971, it issued a contract to Rocketdyne to begin development on the RS-25 engine.

  4. Common Berthing Mechanism - Wikipedia

    en.wikipedia.org/wiki/Common_Berthing_Mechanism

    The collection of Shuttle subsystems and components used to hold and manipulate items in the payload bay, especially items for which flight release (or mating) was planned. Elements included the Shuttle RMS, Payload Retention Latch Assemblies, Grapple Fixtures, Targets, and a CCTV system. See the Payload Bay User's Guide (NASA/NSTS, 2011).

  5. STS-61-C - Wikipedia

    en.wikipedia.org/wiki/STS-61-C

    The mission lasted a total of 6 days, 2 hours, 3 minutes, and 51 seconds. STS-61-C was the last successful Space Shuttle flight before the Challenger disaster, which occurred on January 28, 1986, only 10 days after Columbia ' s return. Accordingly, commander Gibson later called the STS-61-C mission "The End of Innocence" for the Shuttle Program ...

  6. Studied Space Shuttle designs - Wikipedia

    en.wikipedia.org/wiki/Studied_Space_Shuttle_designs

    The external tank and Space Shuttle Solid Rocket Boosters (SRBs) would be combined with a cargo module that took the place of the shuttle orbiter and included the Space Shuttle Main Engines. A ballistic return pod would be used as the main engine structure and carry 2-4 SSMEs as well as mount the payload/booster stage. It would be recovered via ...

  7. Docking and berthing of spacecraft - Wikipedia

    en.wikipedia.org/wiki/Docking_and_berthing_of...

    Berthing of spacecraft can be traced at least as far back as the berthing of payloads into the Space Shuttle payload bay. [10] Such payloads could be either free-flying spacecraft captured for maintenance/return, or payloads temporarily exposed to the space environment at the end of the Remote Manipulator System .

  8. Multi-Purpose Logistics Module - Wikipedia

    en.wikipedia.org/wiki/Multi-Purpose_Logistics_Module

    A Multi-Purpose Logistics Module (MPLM) is a large pressurized container that was used on Space Shuttle missions to transfer cargo to and from the International Space Station (ISS). Two MPLMs made a dozen trips in the Shuttle cargo bay and initially berthed to the Unity and later the Harmony module on the ISS. Once attached, supplies were ...

  9. STS-59 - Wikipedia

    en.wikipedia.org/wiki/STS-59

    The Space Imaging Radar system (SIR-C) was the only part of the payload to be reactivated. The data recorded during the STS-59 mission would fill the equivalent of 20,000 encyclopedia volumes. Payload managers reported that more than 70 million square kilometers of the Earth's surface, including land and sea, have been mapped on this flight.