Characterization of a Radiometer Window for Mars Aftbody Heating Including Ablation Product Deposition Using a Miniature Arc Jet

Miller, Ruth A ; Tang, Chun ; Mc Glaughlin, Mark S ; White, Todd R ; Ho, Thanh S ; Macdonald, Megan E ; Cruden, Brett A

关键词: RADIOMETERS;    TRANSMISSION LOSS;    ENTRY, DESCENT AND LANDING;    MARS LANDING;    AFTERBODIES;    AERODYNAMIC HEATING;    ABLATION;    HEAT FLUX;    HEAT SHIELDING;    THERMAL PROTECTION;    MASS TRANSFER;    SPECTRUM ANALYSIS;    ARC CHAMBERS;    STAGNATION PRESSURE;    CALIBRATING;    MARS 2020 ROVER;   

RP-ID  :  ARC-E-DAA-TN58032

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The Mars Entry, Descent, and Landing Instrumentation 2 (MEDLI2) sensor suite for the Mars 2020 mission includes a radiometer on the backshell to measure the radiative heating during entry into the Martian atmosphere. Thermal Protection System (TPS) ablation products may be deposited on the radiometer window which would degrade the transmission and thus alter the accuracy of the radiometer readings. Testing in NASA Ames Research Center's miniature arc jet (mARC) facility was conducted to deposit TPS ablation products on radiometer windows in an effort to characterize how the ablation products change the window transmission and thus alter radiometer performance. Heat flux and stagnation pressure characterization of the mARC facility in a 90 percent CO2, 10 percent N2 (by mass) Mars-like environment are presented. The spectral transmission of the radiometer windows before and after mARC testing are compared. Additionally, a discussion of how flight-like these test conditions were and future work to further characterize the effect of TPS ablation on radiometer performance are presented.