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Pterodactyl: Non-Propulsive Control System Designs for Future Planetary MissionsAdvances in deployable entry vehicle (DEV) technology, entry guidance, woven thermal protection systems, and affordable launch services make it possible to conceive of entry vehicles that optimize maneuverability, usable payload mass and volume, and operational costs. NASA's Space Technology Mission Directorate is currently funding the authors on a project, Pterodactyl, that is using on-the-fly trajectory design and integrated software and hardware development to investigate non-propulsive entry control systems for precision targeting of mechanical DEVs. The authors recently reported developments of these control systems for an asymmetric DEV to track bank commands for a lunar return entry. For this presentation, the authors will highlight key findings from their studies and propose rapid investigations of applications to future Mars missions such as sample return and asset delivery. Pterodactyl entry vehicle designs are suited to handle sensitive payloads and poised to achieve greater payload mass and volume compared to heritage entry vehicles given a particular launch vehicle. Furthermore, these designs could be adapted to launch on less costly launch vehicles as secondary payloads and could enable missions with high-frequency deployment requirements.







Document ID
20200002483
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Alunni, Antonella
(NASA Ames Research Center Moffett Field, CA, United States)
D'Souza, Sarah N.
(NASA Ames Research Center Moffett Field, CA, United States)
Yount, Bryan C.
(NASA Ames Research Center Moffett Field, CA, United States)
Okolo, Wendy A.
(NASA Ames Research Center Moffett Field, CA, United States)
Margolis, Benjamin W.
(NASA Ames Research Center Moffett Field, CA, United States)
Nikaido, Ben E.
(NASA Ames Research Center Moffett Field, CA, United States)
Hays, Zane B.
(Science and Technology Corp. Moffett Field, CA, United States)
Wong, Veronica M.
(Science and Technology Corp. Moffett Field, CA, United States)
Reddish, Brandon J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
April 17, 2020
Publication Date
April 15, 2020
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN79056
Report Number: ARC-E-DAA-TN79056
Meeting Information
Meeting: Mars Exploration Program Analysis Group (Virtual) Meeting
Location: Online
Country: United States
Start Date: April 15, 2020
Sponsors: NASA Headquarters
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
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