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Optimal battery selection for hybrid rocket engine [PDF]
AIP Conference Proceedings, 2022 In the present paper, the optimal selection of batteries for an electric pump -fed hybrid rocket engine is analyzed. A two -stage Mars Ascent Vehicle, suitable for the Mars Sample Return Mission, is considered as test case. A single engine is employed in the second stage, whereas the first stage uses a cluster of two engines.
Masseni, F, Masseni F.
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Optimal Robust Design of Hybrid Rocket Engines
Springer Optimization and Its Applications, 2016Hybrid rocket engines are flexible, safe, reliable, and low-cost and can be used in many aerospace applications. The engine design and operation are contingent on the type of designated mission and engine design is strictly related to trajectory optimization.
Dario Pastrone +2 more
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Thermoacoustic instabilities in future hybrid rocket engines [PDF]
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 ...
Giraudi, Pietro
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Scalability and dynamic stability of hybrid rocket engines
Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, 2011This paper is divided in two parts. The purpose of the first part is to tackle the problem of geometrical scalability of hybrid rocket engines while the second part of the paper the stability of hybrid rocket motor is investigated using Liapunov theory.
Teodor-Viorel Chelaru
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Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines [PDF]
Journal of Propulsion and Power, 2020 A predictive numerical approach, based on Reynolds-averaged Navier–Stokes simulations including the effects of turbulence, chemistry, fluid/surface interaction, and radiation, has been developed for paraffin-wax/oxygen hybrid rocket engines.
Mario Tindaro Migliorino +2 more
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Optimal propellant control in hybrid rocket engines
31st Joint Propulsion Conference and Exhibit, 1995Paper AIAA 95 ...
COLASURDO, GUIDO +2 more
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Restart transients of hybrid rocket engines.
Journal of Spacecraft and Rockets, 1973Experimental investigation of the problems associated with restarting hybrid rocket motors (i.e., motors wherein a liquid or gaseous oxidizer is injected into the port of a solid fuel grain with subsequent mixing and combustion of the oxidizer and fuel) following a brief period of extinguishment. The results include the finding that the ignition delay
M. A. SARANIERO +2 more
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Characterization of Advanced Hybrid Rocket Engines [PDF]
, 2015 In the last years, the discovery of high regression rate liquefying fuels has generated a renewed interest in hybrid propulsion systems due to some advantages in certain applications compared to solid or liquid rockets. The intrinsic safety, simplicity
Petrarolo, Anna +2 more
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Hybrid Gas Generator for a Staged Hybrid Rocket Engine
Journal of Propulsion and Power, 2017The two-stage combustion hybrid rocket engine with a hybrid gas generator method offers numerous advantages over a solid-propellant gas generator and classical hybrid rocket engines. These advantages include a higher specific impulse in operation, lower lifecycle costs, and lower sensitivity to combustion pressure.
Dongeun Lee, Changjin Lee
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2012
The hybrid rocket engine utilizes a combination of solid rocket and liquid rocket technology to meet some flight mission applications. In terms of performance, cost, availability of materials and safety, the hybrid approach does potentially have some advantages.
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The hybrid rocket engine utilizes a combination of solid rocket and liquid rocket technology to meet some flight mission applications. In terms of performance, cost, availability of materials and safety, the hybrid approach does potentially have some advantages.
openaire +1 more source