Aeroassist Technologies for Small Satellite Missions

Cassell, Alan M ; Dwyer Cianciolo, Alicia M

关键词: AEROASSIST;    AEROCAPTURE;    SAMPLE RETURN MISSIONS;    AEROSHELLS;    DEEP SPACE;    LUNAR GEOLOGY;    MISSION PLANNING;    ORBIT INSERTION;   

RP-ID  :  ARC-E-DAA-TN68228

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Orbit insertion operations that require large V maneuvers using conventional propulsive technologies are mass inefficient and challenging to package within SmallSat form factors such as the popular CubeSat. Aeroassist technologies offer an alternative approach for V maneuvers and could revolutionize the use of SmallSats for exploration missions and increase the science return while reducing costs for orbital or entry missions to Mars, Venus and return to Earth. Aeroassist refers to the use of an atmosphere to accomplish a transportation system function using techniques such as aerobraking, aerocapture, aeroentry, and aerogravity assist. Aeroassist technologies are power efficient and tolerant to the radiation and thermal environment encountered in deep space, and can be integrated around or within SmallSat geometries. This presentation will discuss various Aeroassist technologies including conventional rigid aeroshells, inflatable decelerators, mechanically deployable decelerators and other drag devices and control methods that should be considered by Small Satellite mission design teams.