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  2. Hypergolic propellant - Wikipedia

    en.wikipedia.org/wiki/Hypergolic_propellant

    A hypergolic propellant is a rocket propellant combination used in a rocket engine, whose components spontaneously ignite when they come into contact with each other. The two propellant components usually consist of a fuel and an oxidizer .

  3. Category:Rocket engines using hypergolic propellant - Wikipedia

    en.wikipedia.org/wiki/Category:Rocket_engines...

    This page was last edited on 31 December 2018, at 21:36 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.

  4. Aerozine 50 - Wikipedia

    en.wikipedia.org/wiki/Aerozine_50

    Aerozine 50 is a 50:50 mix by weight of hydrazine and unsymmetrical dimethylhydrazine (UDMH), [1] [2] developed in the late 1950s by Aerojet General Corporation as a storable, high-energy, hypergolic fuel for the Titan II ICBM rocket engines.

  5. RD-270 - Wikipedia

    en.wikipedia.org/wiki/RD-270

    The propellants used are a hypergolic mixture of Unsymmetrical dimethylhydrazine (UDMH) fuel with Dinitrogen tetroxide (N 2 O 4) oxidizer. The chamber pressure was among the highest considered, being about 26 MPa.

  6. SuperDraco - Wikipedia

    en.wikipedia.org/wiki/SuperDraco

    SuperDraco is a hypergolic propellant rocket engine designed and built by SpaceX.It is part of the SpaceX Draco family of rocket engines. A redundant array of eight SuperDraco engines provides fault-tolerant propulsion for use as a launch escape system for the SpaceX Dragon 2, a passenger-carrying space capsule.

  7. YF-20 - Wikipedia

    en.wikipedia.org/wiki/YF-20

    The YF-20 is a Chinese liquid-fuel rocket engine burning N 2 O 4 and UDMH in a gas generator cycle. It is a basic engine which when mounted in a four engine module forms the YF-21. ...

  8. AJ10 - Wikipedia

    en.wikipedia.org/wiki/AJ10

    It was first used in the Delta-A/Able second stage of the Vanguard rocket, in the AJ10-37 configuration. It was initially fueled by nitric acid and UDMH. [2] An AJ10 engine was first fired in flight during the third Vanguard launch, on 17 March 1958, which successfully placed the Vanguard 1 satellite into orbit.

  9. Fregat - Wikipedia

    en.wikipedia.org/wiki/Fregat

    Its liquid propellant engine uses unsymmetrical dimethylhydrazine (UDMH) fuel and dinitrogen tetroxide (N 2 O 4) oxidizer, two hypergolic propellants that spontaneously ignites on contact with each other. With a success rate of 97.3%—including two failures and one partial failure—the Fregat is among the most reliable upper stages worldwide.