hydrogen igniter system

  • 1Space Shuttle main engine — SSME redirect here. For the services field, see Service Science, Management and Engineering infobox rocket engine imsize=250 caption=Space Shuttle Main Engine test firing name=Space Shuttle Main Engine country of origin=United States manufacturer …

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  • 2ISS ECLSS — The interactions between the components of the ISS Environmental Control and Life Support System (ECLSS) The International Space Station Environmental Control and Life Support System (ECLSS) is a life support system that provides or controls… …

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  • 3Apollo 6 — Infobox Space mission mission name = Apollo 6 insignia = Apollo program insignia.png command module = CM 020 mass 25,138 kg service module = SM 014 lunar module = LTA 2R (dummy) mass 11,794 kg booster = Saturn V SA 502 spacecraft name = Apollo… …

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  • 4Apollo 8 — Infobox Space mission mission name = Apollo 8 insignia = Apollo 8 patch.png command module = CM 103 mass 28,817 kg service module = SM 103 lunar module = Lunar Test Article (LTA B) mass 9,026 kg booster = Saturn V SA 503 crew size = 3 launch pad …

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  • 5Bipropellant rocket — A bipropellant rocket engine is a rocket engine that uses two propellants (very often liquid propellants) which are kept separately prior to reacting to form a hot gas to be used for propulsion.In contrast, most solid rockets have single solid… …

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  • 6Ares I — This article is about the Ares I launch vehicle. For other uses, see Ares (disambiguation). Ares I Artist s impression of Ares I launch Function man rated orbital launch vehicle Manufacturer Allian …

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  • 7Combustor — Flame stabilized by cyclone. A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, combustion chamber or flame holder. In a gas turbine engine, the combustor or …

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  • 8Thermal power station — Republika Power Plant, a thermal power station in Pernik, Bulgaria …

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  • 9Rocket engine — RS 68 being tested at NASA s Stennis Space Center. The nearly transparent exhaust is due to this engine s exhaust being mostly superheated steam (water vapor from its propellants, hydrogen and oxygen) …

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  • 10Monopropellant rocket — A monopropellant rocket (or monoprop rocket ) is a rocket that uses a single chemical as its propellant. Contents 1 Chemical reaction monopropellant rockets 2 Solar thermal monopropellant thrusters 3 See also …

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