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Main Achievements of the Rocket Technology Flight Experiment ROTEX-T

机译:火箭科技飞行实验的主要成就圈-T

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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:基于在超音速试验期间聚集的经验Shefex-i和Shefex-II德国航空航天中心(DLR)进行了广泛的仪表飞行实验旋转(火箭技术实验转换)。 Rotex-T于2016年7月19日成功推出,于瑞典北部Kiruna附近的Esrange Space Center 06:05 Am Cest。 RWTH亚琛大学的学生支持了数值模拟项目的设计。 Rotex-T是一种低成本的飞行实验任务,没有惯性测量单元,反应控制和降落伞系统。有效载荷达到了183公里的高度,进行了一个小约446秒的总飞行时间进行了弹道重新入口,并且之后由直升机恢复。具有20Hz,1 kHz,10 kHz和2000 kHz的采样率的独特和模块化的数据采集系统是为Rotex-T开发的,以研究Actionary Aborothermal现象。

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