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Liquid Propellant Rocket Engine

SKU: MD-P00488·Spare Parts & Components·Auf Bestellung

Liquid Propellant Rocket Engine
Liquid Propellant Rocket Engine

Übersicht

YY-2 liquid fuel rocket engine Application areas: hypersonic targets, supersonic targets, unmanned aerial vehicles, retrievable flight demonstrations. Ground specific impulse: 220s Features: Green and non-toxic Storage at room temperature Spontaneous ignition Low cost YY-1 liquid fuel rocket engine Application areas : launch vehicle power, main power for transatmospheric vehicles Fuel: liquid oxygen/kerosene Vacuum specific impulse: 310s Features: Green and non-toxic Multiple ignition Large range of thrust adjustment YY-3 liquid fuel rocket engine Application field: landing deceleration power of return aircraft, aircraft boosting power Ground specific impulse:≮242s Features: Green and non-toxic, normal temperature storage, spontaneous ignition, low cost YY-11 liquid fuel rocket engine Application field : first and second stage power of launch vehicle Fuel: liquid oxygen/kerosene Variable thrust range: 100%~60% Features: large-scale variable thrust, two-way swing after the pump, multiple starts, low cost

Technische Daten

Specifications. Wichtige technische Daten: Application areas hypersonic targets, supersonic targets, unmanned aerial vehicles, retrievable flight demonstrations., Ground specific impulse 220s, Swing angle 6, Reusable times 10 times, Fuel liquid oxygen/kerosene, Vacuum specific impulse 310s, Thrust 7~21KN, Application field landing deceleration power of return aircraft, aircraft boosting power, Variable thrust range 100%~60%, Sea level thrust 42T.

Technische Daten — 1 groups
Wichtige technische Daten: Application areas hypersonic targets, supersonic targets, unmanned aerial vehicles, retrievable flight demonstrations., Ground specific impulse 220s, Swing angle 6, Reusable times 10 times, Fuel liquid oxygen/kerosene, Vacuum specific impulse 310s, Thrust 7~21KN, Application field landing deceleration power of return aircraft, aircraft boosting power, Variable thrust range 100%~60%, Sea level thrust 42T.

Technische Daten

Specifications

Application areas
hypersonic targets, supersonic targets, unmanned aerial vehicles, retrievable flight demonstrations.
Ground specific impulse
220s
Swing angle
6
Reusable times
10 times
Fuel
liquid oxygen/kerosene
Vacuum specific impulse
310s
Thrust
7~21KN
Application field
landing deceleration power of return aircraft, aircraft boosting power
Variable thrust range
100%~60%
Sea level thrust
42T

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