首页> 外文会议>Annual International Telemetering Conference and Technical Exhibition >CALCULATING AERODYNAMIC COEFFICIENTS FOR A NASA APOLLO BODY USING TELEMETRY DATA FROM FREE FLIGHT RANGE TESTING
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CALCULATING AERODYNAMIC COEFFICIENTS FOR A NASA APOLLO BODY USING TELEMETRY DATA FROM FREE FLIGHT RANGE TESTING

机译:使用来自免费飞行范围测试的遥测数据计算NASA Apollo主体的空气动力学系数

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The U.S. Army Research Laboratory (ARL) was requested by the National Aeronautics and Space Administration (NASA) Langley Research Center (LaRC) to perform a free-flight experiment with a telemetry (TM) instrumented sub-scaled Apollo shaped reentry vehicle in order to determine its aerodynamic coefficients. ARL has developed a unique flight diagnostic capability for reconstructing flight trajectory and determining aerodynamic coefficients of projectiles by using sensor data telemetered from free flight experiments. A custom launch package was designed for this experiment that included the Apollo shaped projectile, which housed a modular telemetry unit, and a rapid prototyped sabot. The experiment was able to produce estimates for aerodynamic coefficients that were considered accurate and this technique is appealing to NASA for the development of their spacecraft in the future.
机译:美国陆军研究实验室(ARL)由美国国家航空航天局(NASA)Langley研究中心(LANC)要求使用遥测(TM)仪器被仪表型亚级阿波罗形倒回车辆进行自由飞行试验,以便确定其空气动力学系数。 ARL开发了一种独特的飞行诊断能力,用于重建飞行轨迹并通过使用从自由飞行实验的传感器数据来确定射弹的空气动力学系数。为该实验设计了一种自定义发布包,其中包括Apollo Equiplase射弹,该射弹射弹和快速原型Sabot。该实验能够生产出于准确的空气动力学系数的估计,并且这种技术在未来向美国航空航天局吸引了美国航空航天局的发展。

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