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Executor (rocket engine) : ウィキペディア英語版
Executor (rocket engine)

Executor is a rocket engine developed by ARCA〔ARCA, (Executor Rocket Engine ) (accessed 22 Sept 2014)〕 for use on its Haas rocket series and on IAR 111 Excelsior supersonic airplane. Executor uses kerosene〔http://spacefellowship.com/news/art29703/arca-has-completed-the-first-executor-rocket-engine.html〕 and liquid oxygen as propellants in a gas-generator power cycle.
The injector of Executor is of the pintle type that was first used in the Apollo Program for the lunar module landing engine.
Propellants are fed via a single shaft, dual inducer-impeller turbo-pump. The turbine exhaust gases are used for attitude control of the Haas 2 rocket.
==Variants==

Two versions of the Executor are in development. The Executor engine for the first stage of the Haas 2B and Super Haas launchers and for the IAR-111 Excelsior airplane. The second variant is the Executor Plus engine that it uses a larger exhaust nozzle optimized for vacuum operation. The Executor Plus is used on the Haas 2 air-launched rocket and on the second stage of the Super Haas rocket.〔
(【引用サイトリンク】publisher=ARCA )〕

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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