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Liquid Propellant Rocket Engine

SKU: MD-P00488·Spare Parts & Components·受注生産

Liquid Propellant Rocket Engine
Liquid Propellant Rocket Engine

概要

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

技術仕様

Specifications. 主な仕様: 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。

技術仕様 — 1 groups
主な仕様: 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。

技術仕様

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

対応機体

この部品は以下のプラットフォームに対応します。

適合データの準備中です。機体の型番をお知らせください。

書類