GB1326277A - Rocket propelled missile - Google Patents

Rocket propelled missile

Info

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
Application number
GB5565270A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1326277A publication Critical patent/GB1326277A/en
Expired legal-status Critical Current

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.
GB5565270A 1969-12-05 1970-11-23 Rocket propelled missile Expired GB1326277A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (11)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
GB1326277A (en) Rocket propelled missile
CA965246A (en) Dual thrust level monopropellant spacecraft propulsion system
GB1201547A (en) Communications satellite
GB947751A (en) Improvements relating to navigation control for a propulsive vehicle
GB892246A (en) Improvements relating to rockets
GB988318A (en) Frangible fairings for rocket launchers
GB985229A (en) Rocket
GB1291904A (en) Improvements in and relating to propulsion units for water craft
GB1038466A (en) Control device for adjusting the space position of a space vehicle
GB1087543A (en) Improvements relating to gas-cushion vehicles
GB1156871A (en) Improvements in or relating to Underwater Propulsion Systems for a Water to Air Missile
CA619141A (en) Jet propulsion engine of the compounded ram jet turbo rocket type
GB928322A (en) Improved submarine vessel
CAVALLINO et al. Facility studies of propulsion systems for velocities on the order of 8 km/sec with loads to 50 kgs, and rocket control and guidance systems, volume 1(Using equations of motion to calculate dimensions of rocket propulsion system)
BROSCHK Unconventional nozzles(Plug and spike nozzles applied to rocket propulsion system configurations)
CA886831A (en) Rocket propulsion unit with solid fuel propellant
AU409443B2 (en) Jet propulsion engine thrust deflector
BUCHANAN Design and application of large solid-propellant propulsion systems and comparison of a solid-fuel booster engine with a liquid-fuel engine
BUSCHULTE Use of gasdynamic thrust vector control with solid propellant rocket engines, involving the secondary injection of mass into the main supersonic rocket jet
KINGSBURY et al. On the lobar and longitudinal vibrations of solid propellant rocket motors(Lobar and longitudinal natural vibrations of solid propellant rocket engine with stress and displacement treated by approximate method)
SOTTER et al. Pressure oscillations in solid propellant rocket motors, showing that vortices can be generated by acoustic streaming effects
MORRELL Method for continuous variation of propellant flow and thrust in propulsive devices Patent(Continuous variation of propellant flow and thrust by application of liquid foam flow theory to injection orifice)
BAXTER The application of jet-pumping to liquid injection thrust vector control/litvc/(Jet pumping applied to liquid injection thrust vector control/litvc/ of solid rocket to decrease weights of pressurant, tankage and piping)
STONE Advanced liquid and solid propellant rocket propulsion studies including hybrid motors, nozzle design, additives and thrust chambers
BRAGG et al. The control of the rate of thrust build-up in a liquid-propellant rocket engine used in the blue streak propulsion system

Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees