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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. During lift-off and ascent it supplied the fuel and oxidizer under pressure to the three RS-25 main engines in the orbiter. The ET was jettisoned just over 10 seconds after main engine cut-off…
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Explore the main themes, entities and connections around Space Shuttle external tank. Start with the topic map, then use the sections below for research and deeper semantic analysis.
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Space Shuttle external tank | Burn time | 510 s | 1.00 | infobox |
| Space Shuttle external tank | Country of origin | United States | 1.00 | infobox |
| Space Shuttle external tank | Diameter | 8.4 m (27.6 ft) | 1.00 | infobox |
| Space Shuttle external tank | Gross mass | 760,000 kg (1,680,000 lb) | 1.00 | infobox |
| Space Shuttle external tank | Height | 46.9 m (153.8 ft) | 1.00 | infobox |
| Space Shuttle external tank | Manufacturer | NASA Michoud Assembly Facility, contractor: Martin Marietta, later Lockheed Martin | 1.00 | infobox |
| Space Shuttle external tank | Maximum thrust | 1,254,000 lbf (5,580 kN) | 1.00 | infobox |
| Space Shuttle external tank | Powered by | 3 RS-25 mounted on the orbiter | 1.00 | infobox |
| Space Shuttle external tank | Propellant | LH2/LOX | 1.00 | infobox |
| Space Shuttle external tank | Used on | Space Shuttle | 1.00 | infobox |
| Space Shuttle external tank | related to Core stage of Space Launch System | The Space Launch System | 0.60 | section |
| Space Shuttle external tank | related to Core stage of Space Launch System | SLS | 0.60 | section |
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