RU2015100924A - A way to increase the thrust of a hybrid rocket engine - Google Patents

A way to increase the thrust of a hybrid rocket engine Download PDF

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Publication number
RU2015100924A
RU2015100924A RU2015100924A RU2015100924A RU2015100924A RU 2015100924 A RU2015100924 A RU 2015100924A RU 2015100924 A RU2015100924 A RU 2015100924A RU 2015100924 A RU2015100924 A RU 2015100924A RU 2015100924 A RU2015100924 A RU 2015100924A
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RU
Russia
Prior art keywords
rocket engine
hybrid rocket
thrust
increasing
solid
Prior art date
Application number
RU2015100924A
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Russian (ru)
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RU2598984C2 (en
Inventor
Станислав Михайлович Решетников
Илья Андреевич Зырянов
Артемий Геннадьевич Будин
Александр Павлович Позолотин
Original Assignee
Федеральное государственное бюджетное образовательное учреждение высшего образования "Вятский государственный университет"
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Application filed by Федеральное государственное бюджетное образовательное учреждение высшего образования "Вятский государственный университет" filed Critical Федеральное государственное бюджетное образовательное учреждение высшего образования "Вятский государственный университет"
Priority to RU2015100924/06A priority Critical patent/RU2598984C2/en
Publication of RU2015100924A publication Critical patent/RU2015100924A/en
Application granted granted Critical
Publication of RU2598984C2 publication Critical patent/RU2598984C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)

Abstract

Способ увеличения тяги гибридного ракетного двигателя, включающий изменение массового расхода твердофазного компонента топлива путем влияния на процесс горения, отличающийся тем, что в камере сгорания гибридного ракетного двигателя создают электростатическое поле, увеличивающее тепловой поток к поверхности твердофазного компонента и изменяющее интенсивность процесса диспергирования с помощью высоковольтной системы, включающей источник высоковольтного напряжения и два электрода.A method of increasing the thrust of a hybrid rocket engine, including changing the mass flow rate of the solid-phase component of the fuel by influencing the combustion process, characterized in that an electrostatic field is created in the combustion chamber of the hybrid rocket engine, increasing the heat flux to the surface of the solid-phase component and changing the intensity of the dispersion process using a high-voltage system including a source of high voltage and two electrodes.

Claims (1)

Способ увеличения тяги гибридного ракетного двигателя, включающий изменение массового расхода твердофазного компонента топлива путем влияния на процесс горения, отличающийся тем, что в камере сгорания гибридного ракетного двигателя создают электростатическое поле, увеличивающее тепловой поток к поверхности твердофазного компонента и изменяющее интенсивность процесса диспергирования с помощью высоковольтной системы, включающей источник высоковольтного напряжения и два электрода. A method of increasing the thrust of a hybrid rocket engine, including changing the mass flow rate of the solid-phase component of the fuel by influencing the combustion process, characterized in that an electrostatic field is created in the combustion chamber of the hybrid rocket engine, increasing the heat flux to the surface of the solid-phase component and changing the intensity of the dispersion process using a high-voltage system including a source of high voltage and two electrodes.
RU2015100924/06A 2015-01-12 2015-01-12 Method of increasing hybrid rocket engine thrust RU2598984C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015100924/06A RU2598984C2 (en) 2015-01-12 2015-01-12 Method of increasing hybrid rocket engine thrust

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015100924/06A RU2598984C2 (en) 2015-01-12 2015-01-12 Method of increasing hybrid rocket engine thrust

Publications (2)

Publication Number Publication Date
RU2015100924A true RU2015100924A (en) 2016-07-27
RU2598984C2 RU2598984C2 (en) 2016-10-10

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015100924/06A RU2598984C2 (en) 2015-01-12 2015-01-12 Method of increasing hybrid rocket engine thrust

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2742403C1 (en) * 2020-06-17 2021-02-05 Виктор Федорович Карбушев Method for producing, burning and using fuel from water and solutions thereof

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129562A (en) * 1960-10-21 1964-04-21 United Aircraft Corp Method and means for improving combustion characteristics of solid propellants
US4410470A (en) * 1981-01-07 1983-10-18 The United States Of America As Represented By The Secretary Of The Army Increasing burning rate of solid propellants by electric field effects
RU2175399C2 (en) * 1999-07-29 2001-10-27 Южно-Российский государственный технический университет Method of control of rate of combustion of high-energy condensed system
RU2274761C2 (en) * 2004-02-24 2006-04-20 Государственное образовательное учреждение высшего профессионального образования "Южно-Российский государственный технический университет" (Новочеркасский политехнический институт") Method to control ratio of propellant components in hybrid propellant rocket engine
JP3702348B1 (en) * 2004-10-14 2005-10-05 国立大学法人金沢大学 Solid fuel combustion method, solid fuel combustor, and solid fuel engine using the same

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Publication number Publication date
RU2598984C2 (en) 2016-10-10

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