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COMARS+ Instrumentation Package of the ExoMars Schiaparelli Lander and its Flight Performance

机译:Comars + ExoMars Schiaparelli兰德的仪器包及其飞行性能

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The instrumentation package COMARS+ was part of the back cover instrumentation of the ExoMars Schiaparelli lander and consisted of three COMARS sensors and one broadband radiometer. The aerothermal sensors called COMARS combine four discrete sensors measuring static pressure, total heat flux, temperature and radiative heat flux. The Schiaparelli capsule was launched on top of a Proton launcher on 14~(th) March 2016. The entry into the Martian atmosphere took place on 25~(th) October 2016. All COMARS+ sensors operated nominally during the complete entry phase. But the complete flight data package is not available due to an anomaly that led to the failure of Schiaparelli shortly before landing. Nevertheless, a subset of the COMARS+ flight data was transmitted real-time during the entry phase and was received by the ExoMars 2016 orbiter, with the exception of the plasma blackout phase. The radiative heat flux on the back cover close to the vehicle shoulder was measured successfully for the first time on a Mars entry vehicle. The measured maximum radiative contribution was 61 % of the total heat flux at the first measurement point after the blackout phase and 33 % for the next measured trajectory point 10 seconds later. These measurements confirm recent findings that radiative heating can be a significant portion of the total heating on the back cover during Mars entry.
机译:仪表包彗星+是Exomars Schiaparelli着陆器的背面盖板的一部分,包括三个彗星传感器和一个宽带辐射计。称为彗星的空气感传感器结合了四个离散的传感器,测量静压,总热通量,温度和辐射热通量。 2016年3月14日〜(Th)在Proton发射器上推出了Schiaparelli胶囊。2016年10月的25〜(Th)进入火星氛围。所有彗星+传感器在完整的入境阶段中名字运作。但是,由于异常的异常导致塞加帕利不久在着陆前不久,完整的航班数据包裹不适。然而,彗星+飞行数据的子集在入口阶段进行了实时传输,并且由屈光术2016轨道接收,除了等离子体停电阶段之外。在火星入口车辆上第一次成功地测量靠近车辆肩部的后盖上的辐射热通量。测量的最大辐射贡献是在停电阶段之后的第一个测量点的总热通量的61%,下一个测量的轨迹点10秒后的33%。这些测量结果确认了最近的发现,即在火星入口期间辐射加热可以是后盖上的总热量的重要部分。

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