Pterodactyl: Aerodynamic and Aeroheating Model for a Symmetric Deployable Entry Vehicle with Flaps
Author:
Affiliation:
1. University of California, Davis
2. Science and Technology Corporation
3. Johns Hopkins University Applied Physics Laboratory
4. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference16 articles.
1. High Mass Mars Entry, Descent, and Landing Architecture Assessment
2. Flight Mechanics Modeling and Post-Flight Analysis of ADEPT SR-1
3. Survey of planetary entry guidance algorithms
4. Pterodactyl: Trade Study for an Integrated Control System Design of a Mechanically Deployed Entry Vehicle
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3. Pterodactyl: Effects of 3D Thermal Analysis on the Thermal Protection System Design of a Flap Control System;AIAA SCITECH 2022 Forum;2022-01-03
4. Pterodactyl: Thermal Protection System Design Methodology for a Flap Control System;AIAA SCITECH 2022 Forum;2022-01-03
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