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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 +3 more
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Thrust modulation in hybrid rocket engines
Journal of Propulsion and Power, 1988An experimental investigation of hybrid rocket engines (HRE) is performed to study the throttling performance within a thrust range of 10:1. In order to improve the throttling properties over the entire thrust range, the method of secondary gas injection (gasification) was used. The injection gases were reactive (O2) and inert (N2). High-pressure tests
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2019
Предлагается новый гибридный (комбинированный) ракетный двигатель, на который получен патент Украины («Спосіб комбінування реактивного і прямоточного повітряно-реактивного двигунів». 25.08.2015 ¹100987). Обсуждаются некоторые аспекты его конструкции и работы в сравнении с аналогами.
Semenov, К, Kopiyka, A
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Предлагается новый гибридный (комбинированный) ракетный двигатель, на который получен патент Украины («Спосіб комбінування реактивного і прямоточного повітряно-реактивного двигунів». 25.08.2015 ¹100987). Обсуждаются некоторые аспекты его конструкции и работы в сравнении с аналогами.
Semenov, К, Kopiyka, A
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Hybrid Rocket Engines Design for Materials Characterization
2023Hybrid Rocket Engines (HREs) have generated positive interest in the scientific community due to their ability to combine the special characteristics pertaining to solid and liquid propulsion I [ 1]. Eligible as promising technology enablers for the future of space industry, HREs are valuable for their safe and controlled design nature, simplified ...
Mangioni G. +5 more
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Hybrid rocket engine, theoretical model and experiment
Acta Astronautica, 2011Abstract The purpose of this paper is to build a theoretical model for the hybrid rocket engine/motor and to validate it using experimental results. The work approaches the main problems of the hybrid motor: the scalability, the stability/controllability of the operating parameters and the increasing of the solid fuel regression rate.
Teodor-Viorel Chelaru, Florin Mingireanu
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The Stepped Helix Hybrid Rocket Engine
AIAA AVIATION 2023 Forum, 2023Christopher Glaser +3 more
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Optimal Robust Design of Hybrid Rocket Engines
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.
PASTRONE, Dario Giuseppe +1 more
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Modeling entrainment in Hybrid Rocket Engines
2023Crescenzo, Giorgio +9 more
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Bridging the Technology Gap: Strategies for Hybrid Rocket Engines †
Aerospace, 2023Jouke Hijlkema +2 more
exaly
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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