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Flight Mechanics Modeling and Post-Flight Analysis of ADEPT SR-1

机译:ADEPT SR-1的飞行力学建模和飞行后分析

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Sounding Rocket One (SR-1), the first flight test of the Adaptable Deployable Entry and Placement Technology (ADEPT), was performed on Sept. 12, 2018. ADEPT is a deployable aeroshell that can be stowed during launch and then deployed after launch to increase the drag area of the spacecraft when entering into a planetary atmosphere. The main objectives of the SR-1 flight test were to demonstrate that the ADEPT vehicle can be opened exo-atmospherically and to characterize the stability of the vehicle during atmospheric flight. The SR-1 test vehicle was a 0.7 m diameter 70 degree half-angle, faceted, sphere-cone, which was the primary payload on an UP Aerospace Spaceloft (SL) launch vehicle from the White Sands Missile Range (WSMR). ADEPT successfully separated from the spent booster in its stowed configuration, opened above 100 km altitude, and then landed in the deployed configuration within WSMR. The flight mechanics of the vehicle was modeled pre-flight for performance and range safety predictions. This paper describes the pre-flight ADEPT trajectory simulation and how the flight data compared with the predictions from the simulations.
机译:探空火箭一号(SR-1)是适应性可部署进入和放置技术(ADEPT)的首次飞行测试,于2018年9月12日进行。ADEPT是一种可部署飞机机身,可在发射过程中存放,然后在发射后部署在进入行星大气时增加航天器的阻力区域。 SR-1飞行试验的主要目的是证明ADEPT飞机可以在大气外打开,并表征飞机在大气飞行过程中的稳定性。 SR-1测试车是直径为0.7 m的70度半角多面球形圆锥体,它是UP太空飞船(SL)发射的白沙导弹靶场(WSMR)的主要有效载荷。 ADEPT在其收起配置中成功与废旧助推器分离,在100 km以上的高度打开,然后降落到WSMR内的已部署配置。对该飞行器的飞行力学进行了飞行前建模,以进行性能和范围安全性预测。本文介绍了飞行前ADEPT轨迹模拟,以及如何将飞行数据与模拟预测进行比较。

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