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Main Achievements of the Rocket Technology Flight Experiment ROTEX-T

机译:火箭技术飞行实验ROTEX-T的主要成就

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Based on experience gathered during the hypersonic flight experiments SHEFEX-I and SHEFEX-II the German Aerospace Center (DLR) performed the extensively instrumented flight experiment ROTEX-T (ROcket Technology EXperiment-Transition). ROTEX-T was successfully launched on 19~(th) July 2016 at 06:05 am CEST from the Esrange Space Center near Kiruna in northern Sweden. Students of the RWTH Aachen University supported the design of the project with numerical simulations. ROTEX-T was a low cost flight experiment mission without inertial measurement unit, reaction control and parachute system. The payload reached an altitude of 183 kilometers, performed a ballistic re-entry with a total flight time of approximately 446 seconds and was afterwards recovered by helicopter. An unique and modular data acquisition system with sampling rates of 20 Hz, 1 kHz, 10 kHz and 2000 kHz was developed for ROTEX-T to study also instationary aerothermal phenomena.
机译:根据高超音速飞行实验SHEFEX-I和SHEFEX-II的经验,德国航空航天中心(DLR)进行了仪器广泛的飞行实验ROTEX-T(火箭技术实验转换)。 ROTEX-T于CEST于2016年7月19日至06:05在瑞典北部基律纳附近的Esrange航天中心成功发射。亚琛工业大学的学生通过数值模拟来支持该项目的设计。 ROTEX-T是一种低成本的飞行实验任务,没有惯性测量单元,反作用控制和降落伞系统。该有效载荷达到了183公里的高度,进行了弹道再入,总飞行时间约为446秒,随后被直升飞机收回。为ROTEX-T开发了独特的模块化数据采集系统,其采样率分别为20 Hz,1 kHz,10 kHz和2000 kHz,以研究平稳的空气热现象。

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