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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 ...
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.
Integrated cargo carrier structure ICC frame Astronauts and technicians give a sense of scale to the ICC. Integrated Cargo Carrier (ICC) was a project, started in 1997 by the companies Spacehab and Airbus DS Space Systems (formerly Astrium North America), [1] to develop a family of flight proven and certified cross-the-bay cargo carriers designed to fly inside the Space Shuttle cargo bay ...
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.
Payload bay of the shuttle being loaded inside the cleanroom of the Rotating Service Structure. ICC-VLD1 STS-127 Endeavour carried a wide variety of equipment and cargo in the payload bay, with the largest item being the Kibō Japanese Experiment Module Exposed Facility (JEM EF), and the Kibō Japanese Experiment Logistics Module – Exposed ...
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).
The habitable Spacelab laboratory module comprised a cylindrical environment in the rear of the Space Shuttle orbiter payload bay, connected to the orbiter crew compartment by a tunnel. The laboratory had an outer diameter of 4.12 m (13.5 ft), and each segment a length of 2.7 m (8 ft 10 in).
Special efforts were taken to ensure protection against contamination of the payload bay during the ferry flight. [4] Between January 30 and 31, LDEF was removed from Columbia's payload bay in KSC's Orbiter Processing Facility, placed in a special payload canister, and transported to the Operations and Checkout Building. On February 1, 1990 ...