Search results
Results from the WOW.Com Content Network
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.
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.
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 ...
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 ...
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).
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 ...
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 ...
Other objectives of the flight were to perform the operations necessary to fulfill the requirements of experiments located in SPACEHAB-3 and to fly captively, then deploy and retrieve the Spartan-204 payload. Spartan-204, the Shuttle Pointed Autonomous Research Tool for Astronomy, was a free-flying retrievable platform.