ADEPT, A Mechanically Deployable Re-Entry Vehicle System, Enabling Interplanetary CubeSat and Small Satellite Missions

Cassell, Alan M ; Smith, Brandon ; Wercinski, Paul ; Ghassemieh, Shakib ; Hibbard, Ken ; Nelessen, Adam ; Cutts, James

关键词: AEROCAPTURE;    CUBESATS;    DEPLOYMENT;    EARTH-MOON TRAJECTORIES;    FABRICS;    MISSION PLANNING;    REENTRY VEHICLES;    SMALL SCIENTIFIC SATELLITES;   

RP-ID  :  ARC-E-DAA-TN59976

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

There is growing interest for utilizing Small Satellites beyond low Earth orbit. A number of secondary CubeSat payload missions are planned at Mars, cis-Lunar Space, near Earth objects, and moons of the Gas Giants. Use of smaller systems may enable utilization of otherwise unused capacity of larger "host" missions. Development of re-entry systems that leverage and accommodate Small Satellite technology will substantially expand the range of mission applications by offering the capability for high speed entry or aerocapture at destinations with atmospheres. Deployable entry vehicles (DEVs) offer benefits over traditional rigid aeroshells including volume, mass and payload form factor. The Adaptive Deployable Entry and Placement Technology (ADEPT) offers such a delivery capability for Small Sat or CubeSat orbiter(s), in-situ elements, or landers. The ADEPT system can package with off the shelf CubeSat deployment systems (1U-16U) to offer a delivery capability for a single CubeSat or constellations. Furthermore, ADEPT can deliver the same science payload to a destination with a stowed diameter a factor of 3-4 times smaller than an equivalent rigid aeroshell, alleviating volumetric constraints on the secondary payload accommodation or primary carrier spacecraft bus. This paper will describe ADEPT's current development status and define various interplanetary mission concepts in order to provide guidelines for potential Small Satellite payload developers and mission implementers.