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hypergolic ne demek?

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A rocket propellant combination used in a rocket engine is called hypergolic when the propellants spontaneously ignite when they come
Kaynak: Hypergolic propellant
The Space Shuttle Orbital Maneuvering System (OMS), is a system of hypergolic liquid-propellant rocket engines used on the Space Shuttle
Kaynak: Space Shuttle Orbital Maneuvering System
The 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-10
Draco 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-201
ClF 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 propellants
N 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 tetroxide
high-energy, hypergolic fuel for the Titan II ICBM rocket engines, Aerozine continues in wide use as a rocket fuel , typically with
Kaynak: Aerozine 50
It is used as a rocket propellant in bipropellant rocket engines because it is hypergolic with various oxidizers such as nitrogen
Kaynak: Monomethylhydrazine
If 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 venom
spontaneously in air (cf. hypergolic Examples are iron sulfide and many reactive metals including uranium , when powdered or thinly sliced.
Kaynak: Pyrophoricity
developed 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-Stoff
The Descent Propulsion System (DPS) or LMDE (Lunar Module Descent Engine) is a variable throttle hypergolic rocket engine developed by
Kaynak: Descent Propulsion System
The Ascent Propulsion System (APS) or LMAE (Lunar Module Ascent Engine) is a fixed thrust hypergolic rocket engine developed by Bell
Kaynak: Ascent Propulsion System
throttable hypergolic engine to use LOX /Liquid Methane CH sub 4/sub for NASA Exploration Systems Architecture Study (ESAS) engine testing in 2008
Kaynak: RS-18
This was because T-Stoff and C-stoff are hypergolic propellants: they spontaneously ignite when mixed. Even slight contamination between
Kaynak: T-Stoff
retired in favour of future all-Russian carrier rockets, such as the Angara , and because they were fuelled by toxic hypergolic propellant s
Kaynak: Tsyklon-3
It 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

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