| Finite element analysis of the inflatable re-Entry vehicle experiment (IRVE) L Li, K Gonyea, RD Braun 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015 | 14 | 2015 |
| Propulsion system design for a Martian atmosphere-breathing supersonic retropropulsion engine KC Gonyea, RD Braun, AH Auslender Journal of Propulsion and Power 32 (3), 574-582, 2016 | 12 | 2016 |
| Aerodynamic stability and performance of next-generation parachutes for Mars descent KC Gonyea, CL Tanner, IG Clark, LK Kushner, ET Schairer, RD Braun AIAA Paper 1356, 2013 | 7 | 2013 |
| Aerodynamic stability and performance of next-generation parachutes for Mars entry, descent, and landing K Gonyea, R Braun, CL Tanner, IG Clark, LK Kushner, E Schairer AIAA Aerodynamic Decelerator Systems (ADS) Conference, 1356, 2013 | 3 | 2013 |
| Feasibility and Performance of Atmospheric-Breathing Propulsion for Mars Descent KC Gonyea, RD Braun, AH Auslender Journal of Spacecraft and Rockets 55 (2), 346-355, 2018 | 1 | 2018 |
| Use of the Mars atmosphere to improve the performance of supersonic retropropulsion KC Gonyea Georgia Institute of Technology, 2017 | | 2017 |
