Results 181 to 190 of about 940 (232)
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Hybrid rocket engine, theoretical model and experiment

Acta Astronautica, 2011
Abstract 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
openaire   +1 more source

Thrust modulation in hybrid rocket engines

Journal of Propulsion and Power, 1988
An 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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Hybrid rocket engines: The benefits and prospects

Aerospace Science and Technology, 2007
The review of research avenues for working processes (ignition, combustion, etc.) in hybrid rocket engines (HRE), for thermal protection and power characteristics is stated. Based on conducted design and exploratory studies and design developments, the reasonable fields of application of HRE to launch systems for orbit insertion of payload are ...
N.A. Davydenko   +4 more
openaire   +1 more source

Hybrid rocket engine

Herald of Aeroenginebuilding, 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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Hybrid Rocket Engines

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.
openaire   +1 more source

Evaluation of Paraffin-based Fuels for Hybrid Rocket Engines

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014
This paper summarizes the investigations on the combustion behavior of paraffin-based hybrid rocket fuels with gaseous oxygen (GOX) as oxidizer. Combined experimental activities have been done at the DLR Institute of Space Propulsion in Lampoldshausen and at the Space Propulsion Laboratory (SPLab) of Politecnico di Milano.
Kobald, Mario   +5 more
openaire   +2 more sources

Testing 1kN Paraffin-Based Hybrid Rocket Engine

2019
The present paper describes the design and testing activities carried out on a 1000 N hybrid rocket demonstrator, including a preliminary data assessment. Gaseous oxygen and a paraffin-based solid fuel represent the hybrid propellants. The demonstrator configuration and the design logic are presented first.
D. Cardillo   +6 more
openaire   +2 more sources

Scalability and dynamic stability of hybrid rocket engines

Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011, 2011
This 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
openaire   +1 more source

Numerical modeling of hybrid rocket engine

Aerospace Systems, 2023
Sachin Srivastava   +3 more
openaire   +1 more source

Optimal Robust Design of Hybrid Rocket Engines

2016
Hybrid 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
openaire   +1 more source

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