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Space Shuttle Orbiter
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The Space Shuttle orbiters are the orbital spacecraft of the Space Shuttle program operated by NASA, the space agency of the United States. Each orbiter is a reusable winged "spaceplane", a mixture of rocket, spacecraft, and aircraft. The orbiters carry crews and payloads into Earth orbit, perform on-orbit operations, then re-enter the atmosphere and land like gliders to return their crews and any on board payloads to Earth.
In addition to the crew and payload the reusable orbiter carries most of the main propulsion system, but the propellant for its three main engines is fed from a non-reusable external tank, and two reusable solid rocket boosters help propel both the orbiter and the external tank during the first two minutes of ascent.
Specifications(for Endeavour, OV-105)
- Length: 122.17 ft (37.24 m)
- Wingspan: 78.06 ft (23.79 m)
- Height: 58.58 ft (17.25 m)
- Empty Weight: 151,205 lbs (68,586.6 kg)
- Gross Liftoff Weight: 240,000 lbs (109,000 kg)
- Maximum Landing Weight: 230,000 lbs (104,000 kg)
- Main Engines: Three Rocketdyne Block 2 A SSMEs, each with a sea level thrust of 393,800 lbf (178,624 kgf / 1.75MN)
- Maximum Payload: 55,250 lb (25,061.4 kg)
- Payload Bay dimensions: 15 ft by 60 ft (4.6 m by 18.3 m)
- Operational Altitude: 100 to 520 nm (185 to 1,000 km)
- Speed: 25,404 ft/s (7,743 m/s, 27,875 km/h, 17,321 mph)
- Crossrange: 1,085 nautical miles (2,009.4 km)
- Crew: 6-7 (Commander, Pilot, 4-5 Mission Specialists and/or Payload Specialists), 2 (Commander and Pilot) for minimum.
Flight statisticsSee also
External links
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