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Jérôme Messineo
Jérôme Messineo
HyImpulse Technologies
在 hyimpulse.de 的电子邮件经过验证
标题
引用次数
引用次数
年份
Vortex shedding influence on hybrid rocket pressure oscillations and combustion efficiency
J Messineo, JY Lestrade, J Hijlkema, J Anthoine
Journal of Propulsion and Power 32 (6), 1386-1394, 2016
312016
Performances of a multi-pulsed hybrid rocket engine operating with highly concentrated hydrogen peroxide
J Anthoine, JY Lestrade, J Messineo, S Casu
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4906, 2017
202017
3D miles simulation of a hybrid rocket with swirl injection
J Messineo, JY Lestrade, J Hijlkema, J Anthoine
Space Propulsion 2016, 2016
192016
Development of a catalyst for highly concentrated hydrogen peroxide
JY Lestrade, P Prévot, J Messineo, J Anthoine, S Casu, B Geiger
Space Propulsion 2016, 2016
192016
Reconstructed ballistic data versus wax regression-rate intrusive measurement in a hybrid rocket
J Messineo, K Kitagawa, C Carmicino, T Shimada, C Paravan
Journal of Spacecraft and Rockets 57 (6), 1295-1308, 2020
182020
Theoretical investigation on feedback control of hybrid rocket engines
J Messineo, T Shimada
Aerospace 6 (6), 65, 2019
172019
Hydrodynamic instabilities modeling in hybrid rocket engines
J Messineo, JY Lestrade, J Hijlkema, J Anthoine
Journal of Spacecraft and Rockets 56 (5), 1371-1382, 2019
82019
Development and test of an innovative hybrid rocket combustion chamber
JY Lestrade, J Messineo, J Anthoine, A Musker, F Barato
Proceedings of the 7th European Conference for Aeronautics and Space …, 2017
82017
Hybrid chemical engines: recent advances from sounding rocket propulsion and vision for spacecraft propulsion
JY Lestrade, J Messineo, J Hijlkema, P Prévot, G Casalis, J Anthoine
Aerospace Lab 11, 14 pages, 2016
72016
Prediction of Space and Time Distribution of Wax-based Fuel Regression Rate in a Hybrid Rocket
G Naka, J Messineo, K Kitagawa, C Carmicino, T Shimada
AIAA Propulsion and Energy 2020 Forum, 3768, 2020
42020
O/F ratio measurement for hybrid rocket engine feedback control
J Messineo, K Kitagawa, T Shimada
15th International Conference on Flow Dynamics (ICFD), 2018
42018
Tunable diode laser absorption spectroscopy of CO2 and H2O at 2.7 µm in a scramjet combustor and in exhaust gases of a hybrid rocket motor
AK Mohamed, J Messineo, JY Lestrade, S Defoort, J Soutade, P Viguier
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 3548, 2016
42016
Numerical simulation of a H2O2/PE hybrid rocket motor
J Messineo, JY Lestrade, J Anthoine
6th European Conference for Aerospace Sciences (EUCASS), 2015
42015
Evaluation of radiative heat-transfer effect on Paraffin-wax regression rate in hybrid rocket
G Naka, C Carmicino, J Messineo, K Kitagawa, T Shimada
Journal of Propulsion and Power 39 (2), 258-273, 2023
22023
Modélisation des instabilités hydrodynamiques dans les moteurs-fusées hybrides
J Messineo
INSTITUT SUPERIEUR DE L’AERONAUTIQUE ET DE L’ESPACE (ISAE), 2016
22016
75 kN LOX/PARAFFIN FLIGHT-WEIGHT HYBRID MOTOR DEVELOPMENT
J Messineo, A Petrarolo, V Di Pietrantonio, E Paccagnella, B Oker, ...
8th Space Propulsion Conference 2022, 2022
12022
Introduction to Resistor-Based Sensors for Feedback Control of Hybrid Rocket Engines
J Messineo
第 1 回ハイブリッドロケットシンポジウム 講演集= Proceedings of the 1st Hybrid Rocket …, 2018
12018
Flow field explorations and design improvements of a hybrid rocket motor LOx feed line
DJ Rajendran, M Santhanakrishnan, V Pachidis, J Messineo
Acta Astronautica 225, 273-284, 2024
2024
Prediction of Regression Rate on a Wax Fuel hybrid rocket Considering Radiative effects
GENYA NAKA, J MESSINEO, K KITAGAWA, C CARMICINO, T SHIMADA
宇宙科学技術連合講演会講演集 (CD-ROM) 64, 10, 2020
2020
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