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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 .
An air-breathing engine is thus much more propellant efficient than a rocket engine, because the air serves as reaction mass and oxidizer for combustion which does not have to be carried as propellant, and the actual exhaust speed is much lower, so the kinetic energy the exhaust carries away is lower and thus the jet engine uses far less energy ...
The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet).It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III.
Apogee engines typically use one fuel and one oxidizer. This propellant is usually, but not restricted to, [7] a hypergolic combination such as: N 2 H 4 / N 2 O 4, MMH/ N 2 O 4, UDMH/ N 2 O 4. Hypergolic propellant combinations ignite upon contact within the engine combustion chamber and offer very high ignition reliability, as well as the ...
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.
The RD-0203/4 was the second staged combustion engine in the world, only after the S1.5400, and was also the first staged combustion engine with storable propellants. [ 11 ] On 15 September 1968 the RD-0210, RD-0211 and the RD-0212 module launched the Zond 5 around the Moon on a free return trajectory , that sent the first alive organisms ...
Rocket engines using hydrogen peroxide propellant (3 C, 1 P) Pages in category "Rocket engines using hypergolic propellant" The following 87 pages are in this category, out of 87 total.
It became the propellant for most of the early American rockets and ballistic missiles such as the Atlas, Titan I, and Thor. The Soviets quickly adopted RP-1 for their R-7 missile, but the majority of Soviet launch vehicles ultimately used storable hypergolic propellants. As of 2017, it is used in the first stages of many orbital launchers.