Thermal Environment Modeling Practices for the Descent Trajectory of Lunar Landers

Szerszen, Alexander

关键词: DESCENT;    DESIGN ANALYSIS;    LUNAR ORBITS;    MOON;    PROCEDURES;    THERMAL ENVIRONMENTS;    COMPUTERIZED SIMULATION;    MODELS;    TEMPERATURE EFFECTS;    TRAJECTORY ANALYSIS;   

RP-ID  :  M19-7613-1

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

With the current push to send landers back to the moon, properly modeling the thermal environment for the descent is critical. Descent in this paper is described as: descending from low lunar orbit to touch down on surface. There are several challenges during this period, including: many electronics (such as battery, avionics, transponder, etc…) have higher heat loads due to higher power levels, a significant portion of the view factor to space has been blocked out by the moon making heat rejection less efficient, components that normally do not have direct line of sight to the sun may get exposure due to the lander rotating to align for descent, and thruster firing will dump more heat into the lander. All of these factors combine during the most critical phase of a lander mission make it essential that the thermal environment has been properly set up during design and analysis. This paper presents one method of setting up the thermal environment during descent in Thermal Desktop and will also include some tips and tricks.