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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.
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Development of a Student Hybrid Rocket
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2012Nammo Raufoss AS with the support from Andoya Rocket Range has developed a novel small diameter hybrid rocket, the SHR110, for carrying student experiments and small payloads to 10km altitude approximately. The rocket engine is based on a nitrous oxide hybrid rocket motor providing an environmentally clean alternative to the surplus military rockets ...
Jan Erik Ronningen +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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49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013
The high density polyethylene, as hybrid rocket fuel, has been chosen to be studied. Thermogravimetric analysis allowed to determine an Arrhenius type equation for its regression rate. A flash pyrolysis coupled to GC/MS/FID has been used to observe influence of oxidative environment on pyrolysis byproducts quantity.
Mangeot, Alexandre +2 more
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The high density polyethylene, as hybrid rocket fuel, has been chosen to be studied. Thermogravimetric analysis allowed to determine an Arrhenius type equation for its regression rate. A flash pyrolysis coupled to GC/MS/FID has been used to observe influence of oxidative environment on pyrolysis byproducts quantity.
Mangeot, Alexandre +2 more
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TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKET
Symposium (International) on Combustion, 1963In this paper an effort has been made to survey recent theoretical and experimental work related to several aspects of the hybrid combustion process. It has been found that hybrid combustion is controlled by the rate at which heat can be delivered to the fuel surface, rather than by the surface reaction rates.
G. Marxman, M. Gilbert
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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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Assessment of Using Electric Pumps on Hybrid Rockets
AIAA Propulsion and Energy 2019 Forum, 2019In small hybrid rockets, liquid oxidizer is fed into the combustion chamber by pressurizing the oxidizer tank to achieve the desired injector pressure. However, larger applications employ propellant pumps to keep the propellant tank mass at reasonable levels. Conventionally, pumps are implemented on rockets by means of turbopumps.
Gegeoglu, K. +3 more
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Hybrid Sounding Rocket HEROS: TRL 9
2017The inherent safety of hybrid rocket propulsion offers some unique advantages compared to solid and liquid propellant rocket engines. This makes it especially attractive for space tourism, Micro-launcher and hands-on experiments in the education of students. On November 8th , 2016 at 10:30 a.m.
Kobald, Mario +4 more
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Internal ballistic considerations in hybrid rocket design
2nd Propulsion Joint Specialist Conference, 1966This paper outlines methods for calculating the ballistic behavior of hybrid propellant combinations. The effects of scaling, pressure level, and internal geometric configuration are examined, utilizing a machine analysis that is based upon heat-transfer-limited theory.
C. E. WOOLDRIDGE, R. J. MUZZY
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Model of Hybrid Rocket Combustion in Classical Hybrid Rocket Motors
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013Takakazu Morita +3 more
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