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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 Block 2 version of Starship is 52.1 m (171 ft) tall, 9 m (30 ft) wide, [15] and is composed of four general sections: the engine bay, the oxygen tank, the fuel tank, and the payload bay. [1] The retired Block 1 was constructed in a similar manner, though it was only 50.3 m (165 ft) tall.
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 ...
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 ELCs have a deck size of about 14 feet by 16 feet and spans the width of the space shuttle's payload bay. They are made of steel, coated with UV paint. Each one is capable of providing scientists with a platform and infrastructure to deploy experiments in the vacuum of space without requiring a separate dedicated Earth-orbiting satellite.
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).
As an internal response to the Soviets' engineless Buran orbiter, an unpowered Orbiter was designed at Marshall Space Flight Center. A payload bay segment would be added to the rear of the spacecraft and look very similar to the Space Shuttle Enterprise albeit with a few differences. Most of the equipment was stored in the rear of the craft to ...