Simulation of Combustion in a Hybrid Rocket Engine
, 2023 A numerical investigation on the combustion mechanics of a hybrid rocket engine is performed through unsteady Reynolds-averaged Navier-Stokes simulation. The hybrid rocket engine model is based on an experimental laboratory scale engine design operating on GOX and HDPE as a propellant.
openaire +1 more source
Predictive maintenance programs for aircraft engines based on remaining useful life prediction. [PDF]
Sci RepXue F, Jin G, Tan L, Zhang C, Yu Y.
europepmc +1 more source
Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]
Sensors (Basel)Yan S, Gao Y, Zhang Z, Li Y.
europepmc +1 more source
Metal-organic frameworks as hypergolic additives for hybrid rockets. [PDF]
Chem Sci, 2022 Jobin O +8 more
europepmc +1 more source
Real-time fault diagnosis for propulsion systems [PDF]
Current research toward real time fault diagnosis for propulsion systems at NASA-Lewis is described. The research is being applied to both air breathing and rocket propulsion systems.
Delaat, John C. +3 more
core +1 more source
Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
PLoS OneHuang AM, Xu Y.
europepmc +1 more source
Mechanical design problems associated with turbopump fluid film bearings [PDF]
Most high speed cryogenic turbopumps for liquid propulsion rocket engines currently use ball or roller contact bearings for rotor support. The operating speeds, loads, clearances, and environments of these pumps combine to make bearing wear a limiting ...
Evces, Charles R.
core +1 more source
Magnetohydrodynamic peristaltic flow of hybrid nanofluid in an asymmetric channel with thermal radiation and shape factors: an application of coolant systems. [PDF]
Discov NanoThirunavukarasan K, Sucharitha G.
europepmc +1 more source
Hydrodynamic Instabilities Modeling in Hybrid Rocket Engines
Hydrodynamic Instabilities Modeling in Hybrid Rocket Engines第1回ハイブリッドロケットシンポジウム（2018年6月28日-29日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県 1st Hybrid Rocket Symposium (June 28-29, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 資料番号: SA6000126012 レポート番号: HR-2018 ...
openaire
Journal of Aerospace Technology and ManagementThis work reports the development of an induction melting system for producing paraffin-based fuel units for hybrid rockets. The system is based in oscillating low-frequency magnetic field to generate heat within the material, enabling a precise ...
José Refugio Martínez +8 more
doaj