GB1326277A - Rocket propelled missile - Google Patents
Rocket propelled missileInfo
- Publication number
- GB1326277A GB1326277A GB5565270A GB5565270A GB1326277A GB 1326277 A GB1326277 A GB 1326277A GB 5565270 A GB5565270 A GB 5565270A GB 5565270 A GB5565270 A GB 5565270A GB 1326277 A GB1326277 A GB 1326277A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frame
- missile
- rocket motor
- annular
- rocket
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/023—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F5/00—Liquid springs in which the liquid works as a spring by compression, e.g. combined with throttling action; Combinations of devices including liquid springs
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Support Of The Bearing (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Testing Of Engines (AREA)
Abstract
1326277 Deflecting jets of rocket propulsion motors MESSERSCHMITT - BOLKOWBLOHM GmbH 23 Nov 1970 [5 Dec 1969] 55652/70 Heading B7G A rocket motor 2 is mounted on a missile 1 so that it may be swivelled for thrust vectoring by a structure comprising a frame 14 attached to the missile and formed with an annular member 17 (shown in cross-section), and a frame 15 attached to the rocket motor and, by rods 19 and servomotor 18, to the missile body, the frame 15 having an annular flexible diaphragm secured to the free edges of member 17 the cavity thus formed being optionally filled with liquid 16. Fuel and oxidant for the rocket motor is sup- plied through flexible pipes 10, 11. Springs in- stead of liquid may be inserted in the annular cavity between the member 17 and the diaphragm. For thrust vectoring, servomotors 18 are operated to rock frame 15 about frame 14 through the medium of the flexible diaphragm.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1961049A DE1961049C3 (en) | 1969-12-05 | 1969-12-05 | Suspension for a pivoting rocket engine for missiles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1326277A true GB1326277A (en) | 1973-08-08 |
Family
ID=5753076
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5565270A Expired GB1326277A (en) | 1969-12-05 | 1970-11-23 | Rocket propelled missile |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1961049C3 (en) |
FR (1) | FR2073451B3 (en) |
GB (1) | GB1326277A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2455514C1 (en) * | 2011-04-04 | 2012-07-10 | Николай Борисович Болотин | Multistage booster-rocket, liquid propellant rocket engine and roll nozzle block |
RU2459971C1 (en) * | 2011-03-23 | 2012-08-27 | Николай Борисович Болотин | Carrier rocket, liquid-propellant rocket engine and roll nozzle block |
RU2524483C1 (en) * | 2013-02-20 | 2014-07-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant rocket engine |
RU2527006C1 (en) * | 2013-02-12 | 2014-08-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant four-chamber rocket engine frame |
RU2579293C1 (en) * | 2015-03-24 | 2016-04-10 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant engine with thrust vector control |
RU2626618C1 (en) * | 2016-05-04 | 2017-07-31 | Акционерное общество "Конструкторское бюро химавтоматики" | Twin-chamber liquid propellant engine with controlled thrust vector |
RU173670U1 (en) * | 2015-12-31 | 2017-09-05 | Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" | Generator gas afterburner |
RU2707015C1 (en) * | 2019-03-04 | 2019-11-21 | Акционерное общество "Конструкторское бюро химавтоматики" | Multi-chamber liquid-propellant rocket engine with afterburning with controlled thrust vector |
RU2707997C1 (en) * | 2019-01-29 | 2019-12-03 | Акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant rocket engine with controlled vector of thrust |
RU2739660C1 (en) * | 2020-03-24 | 2020-12-28 | Акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant rocket engine with afterburning with controlled vector of thrust |
RU2768637C1 (en) * | 2021-04-16 | 2022-03-24 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королёва" | Thrust vector control system of a liquid rocket engine |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2451201C1 (en) * | 2010-12-07 | 2012-05-20 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant rocket engine |
RU2536738C1 (en) * | 2014-02-17 | 2014-12-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid fuel rocket motor (lfrm) camera oscillation assembly |
RU2555092C1 (en) * | 2014-06-10 | 2015-07-10 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Rocking assembly of chamber of liquid-propellant engine (lpe) |
RU2563596C1 (en) * | 2014-07-17 | 2015-09-20 | Открытое акционерное общество "НПО Энергомаш имени академика В.П. Глушко" | Liquid propellant rocket engine unit |
RU2559220C1 (en) * | 2014-10-22 | 2015-08-10 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant engine swing assembly |
RU2708014C1 (en) * | 2019-04-25 | 2019-12-03 | Акционерное общество "Конструкторское бюро химавтоматики" | Method for completion of liquid-propellant engine with afterburning with controlled vector of thrust |
-
1969
- 1969-12-05 DE DE1961049A patent/DE1961049C3/en not_active Expired
-
1970
- 1970-11-23 GB GB5565270A patent/GB1326277A/en not_active Expired
- 1970-12-04 FR FR707043766A patent/FR2073451B3/fr not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2459971C1 (en) * | 2011-03-23 | 2012-08-27 | Николай Борисович Болотин | Carrier rocket, liquid-propellant rocket engine and roll nozzle block |
RU2455514C1 (en) * | 2011-04-04 | 2012-07-10 | Николай Борисович Болотин | Multistage booster-rocket, liquid propellant rocket engine and roll nozzle block |
RU2527006C1 (en) * | 2013-02-12 | 2014-08-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant four-chamber rocket engine frame |
RU2524483C1 (en) * | 2013-02-20 | 2014-07-27 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant rocket engine |
RU2579293C1 (en) * | 2015-03-24 | 2016-04-10 | Открытое акционерное общество "Конструкторское бюро химавтоматики" | Liquid propellant engine with thrust vector control |
RU173670U1 (en) * | 2015-12-31 | 2017-09-05 | Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" | Generator gas afterburner |
RU2626618C1 (en) * | 2016-05-04 | 2017-07-31 | Акционерное общество "Конструкторское бюро химавтоматики" | Twin-chamber liquid propellant engine with controlled thrust vector |
RU2707997C1 (en) * | 2019-01-29 | 2019-12-03 | Акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant rocket engine with controlled vector of thrust |
RU2707015C1 (en) * | 2019-03-04 | 2019-11-21 | Акционерное общество "Конструкторское бюро химавтоматики" | Multi-chamber liquid-propellant rocket engine with afterburning with controlled thrust vector |
RU2739660C1 (en) * | 2020-03-24 | 2020-12-28 | Акционерное общество "Конструкторское бюро химавтоматики" | Liquid-propellant rocket engine with afterburning with controlled vector of thrust |
RU2768637C1 (en) * | 2021-04-16 | 2022-03-24 | Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королёва" | Thrust vector control system of a liquid rocket engine |
Also Published As
Publication number | Publication date |
---|---|
DE1961049B2 (en) | 1974-08-29 |
FR2073451B3 (en) | 1973-08-10 |
DE1961049A1 (en) | 1971-06-09 |
DE1961049C3 (en) | 1975-04-17 |
FR2073451A7 (en) | 1971-10-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |