RU2014132047A - METHOD AND DEVICE FOR STAND EXERCISE AND DISPOSAL OF A ROCKET ENGINE OF SOLID FUEL - Google Patents

METHOD AND DEVICE FOR STAND EXERCISE AND DISPOSAL OF A ROCKET ENGINE OF SOLID FUEL Download PDF

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Publication number
RU2014132047A
RU2014132047A RU2014132047A RU2014132047A RU2014132047A RU 2014132047 A RU2014132047 A RU 2014132047A RU 2014132047 A RU2014132047 A RU 2014132047A RU 2014132047 A RU2014132047 A RU 2014132047A RU 2014132047 A RU2014132047 A RU 2014132047A
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RU
Russia
Prior art keywords
disposal
solid fuel
screen
rocket engine
stand
Prior art date
Application number
RU2014132047A
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Russian (ru)
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RU2604156C2 (en
Inventor
Константин Александрович Ваганов
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Константин Александрович Ваганов
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Priority to RU2014132047/06A priority Critical patent/RU2604156C2/en
Publication of RU2014132047A publication Critical patent/RU2014132047A/en
Application granted granted Critical
Publication of RU2604156C2 publication Critical patent/RU2604156C2/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
    • F02K9/96—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by specially adapted arrangements for testing or measuring

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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)
  • Investigating Or Analyzing Materials Using Thermal Means (AREA)

Abstract

1. Способ стендовой отработки и утилизации ракетного двигателя твердого топлива, включающий установку снаряженного двигателя на силовой пол с упором его передней части в упорный бык, запуск, измерение параметров работы, отличающийся тем, что перед испытанием напротив каждого сопла на основание стенда устанавливают и закрепляют (например сваркой) газоотражатель так, что его экран расположен под углом 45±5° к оси стенда.2. Устройство для стендовой отработки и утилизации ракетного двигателя твердого топлива, состоящее из рамы сваренной из металлического уголка и экрана (металлического листа), отличающееся тем, что устройство легко устанавливается и закрепляется в любом необходимом месте, и его экран покрыт огнестойким материалом, например асбестовым полотном как минимум в один слой.1. The method of bench testing and disposal of a solid fuel rocket engine, including installing an equipped engine on the power floor with the front of the bull resting on the bull, starting, measuring operation parameters, characterized in that before testing, opposite each nozzle, they are installed and fixed on the stand base ( for example, by welding) a gas deflector so that its screen is located at an angle of 45 ± 5 ° to the axis of the stand. 2. A device for bench testing and disposal of a solid fuel rocket engine, consisting of a frame welded from a metal corner and a screen (metal sheet), characterized in that the device is easily installed and fixed in any necessary place, and its screen is covered with a fire-resistant material, such as asbestos cloth at least one layer.

Claims (2)

1. Способ стендовой отработки и утилизации ракетного двигателя твердого топлива, включающий установку снаряженного двигателя на силовой пол с упором его передней части в упорный бык, запуск, измерение параметров работы, отличающийся тем, что перед испытанием напротив каждого сопла на основание стенда устанавливают и закрепляют (например сваркой) газоотражатель так, что его экран расположен под углом 45±5° к оси стенда.1. The method of bench testing and disposal of a solid fuel rocket engine, including installing an equipped engine on the power floor with the front of the bull resting on the bull, starting, measuring operation parameters, characterized in that before testing, opposite each nozzle, they are installed and fixed on the stand base ( for example by welding) a gas deflector so that its screen is located at an angle of 45 ± 5 ° to the axis of the stand. 2. Устройство для стендовой отработки и утилизации ракетного двигателя твердого топлива, состоящее из рамы сваренной из металлического уголка и экрана (металлического листа), отличающееся тем, что устройство легко устанавливается и закрепляется в любом необходимом месте, и его экран покрыт огнестойким материалом, например асбестовым полотном как минимум в один слой. 2. A device for bench testing and disposal of a solid fuel rocket engine, consisting of a frame welded from a metal corner and a screen (metal sheet), characterized in that the device is easily installed and fixed in any necessary place, and its screen is covered with a fire-resistant material, such as asbestos canvas at least one layer.
RU2014132047/06A 2014-08-01 2014-08-01 Method and device for bench testing solid propellant rocket engine RU2604156C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014132047/06A RU2604156C2 (en) 2014-08-01 2014-08-01 Method and device for bench testing solid propellant rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014132047/06A RU2604156C2 (en) 2014-08-01 2014-08-01 Method and device for bench testing solid propellant rocket engine

Publications (2)

Publication Number Publication Date
RU2014132047A true RU2014132047A (en) 2016-02-20
RU2604156C2 RU2604156C2 (en) 2016-12-10

Family

ID=55313483

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014132047/06A RU2604156C2 (en) 2014-08-01 2014-08-01 Method and device for bench testing solid propellant rocket engine

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RU (1) RU2604156C2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111219267A (en) * 2018-11-23 2020-06-02 北京航天试验技术研究所 High-temperature high-speed jet flow deflection device
CN113586288A (en) * 2021-09-28 2021-11-02 南京理工大学 High-speed rotating platform test device for solid rocket engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2925013A (en) * 1956-05-01 1960-02-16 North American Aviation Inc Rocket engine assembly testing and launching apparatus
US3797787A (en) * 1971-04-17 1974-03-19 Nippon Steel Corp Jet engine blast fence
US4541594A (en) * 1980-12-22 1985-09-17 General Dynamics Corporation Takeoff and landing platform for V/STOL airplane
US4733751A (en) * 1985-12-27 1988-03-29 General Dynamics, Pomona Division Rocket exhaust disrupter
RU26429U1 (en) * 2002-05-30 2002-12-10 Киреев Валерий Николаевич FIRE-PROTECTIVE COATING OF "POLYKROV ASB"
RU90548U1 (en) * 2009-07-20 2010-01-10 Открытое акционерное общество Конструкторское бюро транспортного машиностроения (ОАО КБТМ) Combat vehicle of a multiple launch rocket system on a tracked chassis

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111219267A (en) * 2018-11-23 2020-06-02 北京航天试验技术研究所 High-temperature high-speed jet flow deflection device
CN113586288A (en) * 2021-09-28 2021-11-02 南京理工大学 High-speed rotating platform test device for solid rocket engine
CN113586288B (en) * 2021-09-28 2022-01-21 南京理工大学 High-speed rotating platform test device for solid rocket engine

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Publication number Publication date
RU2604156C2 (en) 2016-12-10

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Effective date: 20190802