Assertion: space shuttle's tank | /r/HasProperty | et
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Source sentences:
text: Space Shuttle components include the Orbiter Vehicle (OV) with three clustered Rocketdyne RS-25 main engines, a pair of recoverable solid rocket boosters (SRBs), and the expendable external tank (ET) containing liquid hydrogen and liquid oxygen.
text: At launch, it consisted of the orbiter, which contained the crew and payload, the external tank (ET), and the two solid rocket boosters (SRBs).:363
text: The Space Shuttle external tank (ET) carried the propellant for the Space Shuttle Main Engines, and connected the orbiter vehicle with the solid rocket boosters.
text: The Space Shuttle external tank (ET) was the component of the Space Shuttle launch vehicle that contained the liquid hydrogen fuel and liquid oxygen oxidizer.
text: At 81.7 seconds after launch from Kennedy Space Center's LC-39-A, a suitcase-sized piece of foam broke off from the external tank (ET), striking Columbia's left wing reinforced carbon-carbon (RCC) panels.
text: With the first vertical motion of the vehicle, the gaseous hydrogen vent arm retracted from the external tank (ET) but failed to latch back.
text: At launch, the space shuttle system, or ‘stack’ comprises three main components: a black-and-white orbital vehicle (OV) containing payload and crew, as well as the space shuttle main engines (SSMEs) and orbital manoeuvring engines (OMEs), two white solid rocket boosters (SRBs) and an orange external tank (ET) carrying liquid fuel oxidizer and liquid hydrogen.
text: Shuttle components included the Orbiter Vehicle (OV) with three clustered Rocketdyne RS-25 main engines, a pair of recoverable solid rocket boosters (SRBs), and the expendable external tank (ET) containing liquid hydrogen and liquid oxygen.
text: The engines, drawing propellant from the Space Shuttle external tank (ET) via the orbiter's main propulsion system (MPS), were ignited at T−6.6 seconds prior to liftoff (with each ignition staggered by 120 ms), which allowed their performance to be checked prior to ignition of the Space Shuttle Solid Rocket Boosters (SRBs), which committed the shuttle to the launch.
text: The RS-25 engines used a combination of liquid hydrogen and liquid oxygen (LOX) from the external tank (ET), as the orbiter did not have room for internal fuel tanks.
text: The Gaseous Oxygen Vent Arm positioned a hood, often called the "Beanie Cap", over the top of the external tank (ET) nose cone during fueling.[when?]
text: After 8 minutes and 34 seconds Mission Elapsed Time (MET) the main engines were shut down (MECO, at altitude 388,000 feet (118,000 m)) and the external tank (ET) was jettisoned 18 seconds later to eventually break up and impact in the Indian Ocean.
text: As of May 2009, DIRECT revolves a notional series of vehicles, dubbed "Jupiter", that would use an external tank (ET) derived core stage powered by three or four Space Shuttle Main Engines (SSMEs), plus a pair of standard four-segment SRBs.
text: The orthogrid was carved from a single metal plate to be part of the wall of a super-lightweight space shuttle external tank (ET).
text: Space Shuttle components include the Orbiter Vehicle (OV) with three clustered Rocketdyne RS-25 main engines, a pair of recoverable solid rocket boosters (SRBs), and the expendable external tank (ET) containing liquid hydrogen and liquid oxygen.
text: At launch, it consisted of the orbiter, which contained the crew and payload, the external tank (ET), and the two solid rocket boosters (SRBs).:363
text: The Space Shuttle external tank (ET) carried the propellant for the Space Shuttle Main Engines, and connected the orbiter vehicle with the solid rocket boosters.