Results 161 to 170 of about 450 (188)
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Thermoacoustic instabilities in future hybrid rocket engines
This thesis investigates the thermoacoustic behaviour of the PB1–HX3 subsystem—comprising a preburner and heat exchanger—within SABRE (Synergetic Air-Breathing Rocket Engine), a single-stage-to-orbit propulsion concept by Reaction Engines Ltd. SABRE integrates advanced heat exchangers with conventional turbomachinery to operate in air-breathing and ...openaire +1 more source
Numerical simulation of hybrid rocket engine flowfields
2013Numerical simulations of the flow in a GOX/HTPB hybrid rocket engine are carried out with a Reynolds averaged Navier-Stokes solver including detailed gas surface interaction mass and energy balances. Global mechanisms are considered for the gas-phase chemistry.
BIANCHI, DANIELE +3 more
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Labscale hybrid uncertainty analysis (hybrid rocket engines)
31st Joint Propulsion Conference and Exhibit, 1995B Greiner, R Frederick, r
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Uncertainty Analysis and Robust Design for Hybrid Rocket Engines
2018 Joint Propulsion Conference, 2018Casalino, Lorenzo +2 more
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Numerical study of the hybrid rocket engine
Aerospace SystemsC. Ommounica +2 more
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Development of a Nytrox-Paraffin Hybrid Rocket Engine
AIAA Propulsion and Energy 2020 Forum, 2020Vignesh Sella +9 more
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Experimental Demonstration of the Vacuum Specific Impulse of a Hybrid Rocket Engine
Journal of Spacecraft and Rockets, 2017Jean-Yves Lestrade, Jérôme Anthoine
exaly