A rocket propellant combination used in a rocket engine is called
hypergolic when the propellants spontaneously ignite when they come
Kaynak: Hypergolic propellantThe AJ-10 or AJ10 is a
hypergolic rocket engine manufactured by Aerojet . It has been used to propel the upper stages of several carrier
Kaynak: AJ-10Draco is a group of
hypergolic rocket engines (known as thrusters) designed by SpaceX for use on their Dragon spacecraft the upper stage
Kaynak: Draco (rocket engine family)The TR-201 or TR201 is a
hypergolic pressure-fed rocket engine . It was used to propel the upper stage of the Delta rocket from 1972 to
Kaynak: TR-201ClF sub 3/sub MMH /N sub 2/sub H sub 4/sub /N 2 H 5 NO 3 55/26/19
hypergolic 2789 2.97 3407 1.42 1739 3274 3.01 3413 1.42 1739 N sub 2/sub
Kaynak: Liquid rocket propellantsN 2 O 4 is
hypergolic with various forms of hydrazine , i.e., they burn on contact without a separate ignition source, making them
Kaynak: Dinitrogen tetroxidehigh-energy,
hypergolic fuel for the Titan II ICBM rocket engines, Aerozine continues in wide use as a rocket fuel , typically with
Kaynak: Aerozine 50It is used as a rocket propellant in bipropellant rocket engines because it is
hypergolic with various oxidizers such as nitrogen
Kaynak: MonomethylhydrazineIf the fuel and oxidizer are
hypergolic , they burn on contact; non-
hypergolic fuels require an igniter. Multiple burns can be conducted
Kaynak: Pressure-fed cycle (rocket)for a liquid rocket fuel composed of a dangerous combination of nitric acid and hydrazine - specifically,
hypergolic UDMH -nitric acid .
Kaynak: Devil's venomspontaneously in air (cf.
hypergolic Examples are iron sulfide and many reactive metals including uranium , when powdered or thinly sliced.
Kaynak: Pyrophoricitydeveloped for use with T-Stoff (a high test peroxide ), as an oxidizer, which together with C-Stoff as the fuel, forms a
hypergolic mixture . |
Kaynak: C-StoffThe Descent Propulsion System (DPS) or LMDE (Lunar Module Descent Engine) is a variable throttle
hypergolic rocket engine developed by
Kaynak: Descent Propulsion SystemThe Ascent Propulsion System (APS) or LMAE (Lunar Module Ascent Engine) is a fixed thrust
hypergolic rocket engine developed by Bell
Kaynak: Ascent Propulsion Systemthrottable
hypergolic engine to use LOX /Liquid Methane CH sub 4/sub for NASA Exploration Systems Architecture Study (ESAS) engine testing in 2008
Kaynak: RS-18This was because T-Stoff and C-stoff are
hypergolic propellants: they spontaneously ignite when mixed. Even slight contamination between
Kaynak: T-Stoffretired in favour of future all-Russian carrier rockets, such as the Angara , and because they were fuelled by toxic
hypergolic propellant s
Kaynak: Tsyklon-3It delivered 37.3 kN (8380 lbf) and ran on a mix of TG-02
hypergolic kerosene and AK-20 oxidizer (nitric acid). The fuel pumps were
Kaynak: Dushkin S-155