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 PDFInfo
- 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
- Authority
- RU
- Russia
- Prior art keywords
- disposal
- solid fuel
- screen
- rocket engine
- stand
- Prior art date
Links
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
Landscapes
- 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)
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 |
Country Status (1)
Country | Link |
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RU (1) | RU2604156C2 (en) |
Cited By (2)
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)
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 |
-
2014
- 2014-08-01 RU RU2014132047/06A patent/RU2604156C2/en not_active IP Right Cessation
Cited By (3)
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 |
Also Published As
Publication number | Publication date |
---|---|
RU2604156C2 (en) | 2016-12-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20190802 |