Inverse heat transfer method applied to capacitively cooled rocket thrust chambers N Perakis, OJ Haidn International Journal of Heat and Mass Transfer 131, 150-166, 2019 | 65 | 2019 |
Heat Transfer and Combustion Simulation of Seven-Element / Rocket Combustor N Perakis, D Rahn, OJ Haidn, D Eiringhaus Journal of Propulsion and Power 35 (6), 1080-1097, 2019 | 54 | 2019 |
Project Lyra: Sending a spacecraft to 1I/’Oumuamua (former A/2017 U1), the interstellar asteroid AM Hein, N Perakis, TM Eubanks, A Hibberd, A Crowl, K Hayward, ... Acta Astronautica 161, 552-561, 2019 | 54 | 2019 |
Data-assisted combustion simulations with dynamic submodel assignment using random forests WT Chung, AA Mishra, N Perakis, M Ihme Combustion and Flame 227, 172-185, 2021 | 47 | 2021 |
Qualitative and quantitative comparison of RANS simulation results for a 7-element GOX/GCH4 rocket combustor N Perakis, OJ Haidn, D Eiringhaus, D Rahn, S Zhang, Y Daimon, S Karl, ... 2018 Joint Propulsion Conference, 4556, 2018 | 45 | 2018 |
Heat flux evaluation in a multi-element CH4/O2 rocket combustor using an inverse heat transfer method N Perakis, J Strauß, OJ Haidn International Journal of Heat and Mass Transfer 142, 118425, 2019 | 29 | 2019 |
Combining magnetic and electric sails for interstellar deceleration N Perakis, AM Hein Acta Astronautica 128, 13-20, 2016 | 29 | 2016 |
Heat Flux Evaluation Methods for a Single Element Heat Sink Chamber MP Celano, S Silvestri, PJ Dominic, N Perakis, F Schily, O Haidn, ... 6th European Conference for Aeronautics and Space Sciences (EUCASS), 2015 | 27 | 2015 |
Project Dragonfly: A feasibility study of interstellar travel using laser-powered light sail propulsion N Perakis, LE Schrenk, J Gutsmiedl, A Koop, MJ Losekamm Acta Astronautica 129, 316-324, 2016 | 26 | 2016 |
Interstellar now! Missions to explore nearby interstellar objects AM Hein, TM Eubanks, M Lingam, A Hibberd, D Fries, J Schneider, ... Advances in Space Research 69 (1), 402-414, 2022 | 23 | 2022 |
CFD-analysis of the effect of a cooling film on flow and heat transfer characteristics in a GCH4/GOX rocket combustion chamber A Sternin, N Perakis, MP Celano, M Tajmar, O Haidn Space Propulsion Conference 2018, 2018 | 22 | 2018 |
Comparison of single and multi-injector GOC/CH4 combustion chambers MP Celano, S Silvestri, C Bauer, N Perakis, G Schlieben, OJ Haidn 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4990, 2016 | 21 | 2016 |
Emission imaging and CFD simulation of a coaxial single-element GOX/GCH4 rocket combustor FF Winter, N Perakis, OJ Haidn 2018 Joint Propulsion Conference, 4764, 2018 | 20 | 2018 |
Hot firing of a N2O/C2H4 premixed green propellant: First combustion tests and results L Werling, N Perakis, S Müller, A Hauck, H Ciezki, S Schlechtriem Space Propulsion Conference, 2016 | 20 | 2016 |
Heat flux and temperature evaluation in a rectangular multi-element GOX/GCH4 combustion chamber using an inverse heat conduction method N Perakis, MP Celano, OJ Haidn 7th European Conference for Aerospace Sciences, 2017 | 19 | 2017 |
Development of a non-adiabatic Flamelet model for reacting flows with heat loss N Perakis, C Roth, OJ Haidn Space Propulsion Conference 2018, 2018 | 17 | 2018 |
Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model N Perakis, OJ Haidn Acta Astronautica 174, 254-269, 2020 | 16 | 2020 |
Investigation of CO recombination in the boundary layer of CH4/O2 rocket engines N Perakis, OJ Haidn, M Ihme Proceedings of the Combustion Institute 38 (4), 6403-6411, 2021 | 15 | 2021 |
Numerical Calculation of Heat Flux Profiles in a N2O/C2H4 Premixed Green Propellant Combustor using an Inverse Heat Conduction Method N Perakis, L Werling, H Ciezki, S Schlechtriem Space Propulsion Conference 1 (5), 2016 | 15 | 2016 |
Experimental investigations based on a demonstrator unit to analyze the combustion process of a nitrous oxide/ethene premixed green bipropellant L Werling, N Perakis, B Hochheimer, H Ciezki, S Schlechtriem 5th CEAS Air & Space Conference 7 (11), 2015 | 15 | 2015 |