Liquid Propellant Rocket Engine
SKU: MD-P00488·Spare Parts & Components·受注生産


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。