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Reusable Sounding Rocket Engine Design and Manufacturing Status of Development Engine and Components

机译:可重复使用的探空火箭发动机的设计和开发引擎及其组件的制造状况

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Reusable Sounding Rocket is under development in Japan. Main engines of this LOX/LH2 system hiresexpander bleed cycle, whichi is Japanese unique system in the world. This engine will demonstrate thefeatures of 40 to 100 percent continuous throttling capability, restart, health monitoring, idle mode andeasy operation. Detail design of the development engine and its components has been almost finished andthe hardware will be ready for ground engineering tests at Kakuda JAXA facility in the autumn of this year.This paper describes status of design and manufacturing of development engine and components includingcombustion chamber, injector, igniter, turbopumps, valves and controllers.
机译:可重复使用的“探空火箭”在日本正在开发中。此LOX / LH2系统雇用的主要引擎 扩展器放气循环,这是世界上日本独有的系统。该引擎将演示 具有40%到100%的连续节流能力,重新启动,运行状况监视,空闲模式和 操作简单。开发引擎及其组件的详细设计已接近完成,并且 硬件将在今年秋天准备在角田JAXA设施进行地面工程测试。 本文介绍了开发引擎和组件的设计和制造状态,包括 燃烧室,喷油器,点火器,涡轮泵,阀门和控制器。

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