Speaker
Description
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 14th March 2016. The entry into the Martian atmosphere took place on 25th 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 (see Figure 1). 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 more than 60 % of the total heat flux at the first measurement point after the blackout phase. These measurements confirm recent findings that radiative heating can be a significant portion of the total heating on the back cover during Mars entry. In addition measured total heat flux rate on the back cover has been compared with the stagnation point heat flux rate.
Summary
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 14th March 2016. The entry into the Martian atmosphere took place on 25th 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 (see Figure 1). 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 more than 60 % of the total heat flux at the first measurement point after the blackout phase. These measurements confirm recent findings that radiative heating can be a significant portion of the total heating on the back cover during Mars entry. In addition measured total heat flux rate on the back cover has been compared with the stagnation point heat flux rate.
