| Hybrid rockets with mixed N2O/CO2 oxidizers for Mars Ascent Vehicles O Kara, H Karakaş, AM Karabeyoglu Acta Astronautica 175, 254-267, 2020 | 20 | 2020 |
| Performance Enhancing Additives for Hybrid Rockets H Karakas, O Kara, I Ozkol, AM Karabeyoglu AIAA Propulsion and Energy 2019 Forum, 3922, 2019 | 8 | 2019 |
| Communication Architecture and International Policy Recommendations Enabling the Development of Global CubeSat Space Networks O Kara, SGCCSW Group International Astronautical Congress, 2015 | 7 | 2015 |
| Influence of micro-aluminum addition to paraffin-based fuels on graphite nozzle erosion rate H Karakas, O Kara, B Kahraman, BN Eren, I Ozkol, A Karabeyoglu AIAA Propulsion and Energy 2020 Forum, 3752, 2020 | 4 | 2020 |
| Ignition Capability of CO2 in Hybrid Rockets for Mars Ascent Vehicles O Kara, A Karabeyoglu Phd thesis, Koç University, 2021 | 3 | 2021 |
| Experimental study of lunar-based hybrid rocket engine U Yelken, A Yalcintas, O Kara, M Baysal, MA Karabeyoglu AIAA Propulsion and Energy 2021 Forum, 3507, 2021 | 3 | 2021 |
| Propulsion System Design for Mars Ascent Vehicles by using the In-Situ CO2 O Kara, M Karpat, MA Karabeyoglu AIAA Propulsion and Energy 2021 Forum, 3248, 2021 | 3 | 2021 |
| Small Satellite Architecture Optimization: Electric Propulsion Moon Imaging Mission O Kara, AM Karabeyoglu AIAA SPACE 2015 Conference and Exposition, 4600, 2015 | 3 | 2015 |
| Hybrid Propulsion System: Novel Propellant Design for Mars Ascent Vehicles O Kara, A Karabeyoglu Propulsion-New Perspectives and Applications, 2021 | 2 | 2021 |
| Emerging Small Satellite Operations In Turkey: Interplanetary Mission Infrastructure and Bene ts in the Space Sector O Kara, C Kilic International Astronautical Congress, 2015 | 2 | 2015 |
| Experimental Test of N2O/CO2 Oxidizer Mixture with Paraffin based Aluminum Fuel for Mars Ascent Vehicles O Kara, H Karakas, AM Karabeyoglu AIAA Propulsion and Energy 2019 Forum, 3923, 2019 | 1 | 2019 |
| System-level optimization approach for small satellite moon missions by using electric propulsion and mission cost survey for Turkish space economy O Kara Koç University, 2016 | 1 | 2016 |
| Comprehensive Study of Small Satellite Moon Missions: Architecture Design, Electric Propulsion System Optimization and Cost Analysis O Kara, C Kilic International Astronautical Congress, 2015 | 1 | 2015 |
| Future Mars Mission Demonstration with Gamification and Socioeconomic Traits: Next Generation Workforce Development and Self-Knowledge Management O Kara AIAA SPACE 2015 Conference and Exposition, 4652, 2015 | 1 | 2015 |
| In-Situ Propellant Design for Mars Ascent Vehicles Room Space Journal 27 (1), 74, 2021 | | 2021 |
| Ignition Boundary of CO2 in Hybrid Rockets for Mars Ascent Vehicles KOC University, 2021 | | 2021 |
| Mars Ascent Vehicle Propulsion System Design By Using CO2 As An In-Situ Oxidizer Space Propulsion Conference, 2021 | | 2021 |
| An Experimental Study on Predicting the Mass Flow Rate of Self-Pressurizing Oxidizers Through Injectors M Karpat, O Kara, MA Karabeyoglu AIAA Propulsion and Energy 2021 Forum, 3512, 2021 | | 2021 |
| Understanding Regression Rate Characteristics of CO2 as an oxidizer compound in Paraffin Based Hybrid Rocket Motors International Astronautical Congress 2020, 2020 | | 2020 |
| Performance Analysis of N2O/CO2 Oxidizer Mixture with Paraffin based Micro-Aluminum Fuel for Mars Ascent Vehicles O Kara, H Karakas, AM Karabeyoglu, B Kahraman, B Eren 70th International Astronautical Congress, 2019 | | 2019 |
Hakki KarakasVerified email at stanford.edu
