EP0128337A3 - Propulsive nozzle system - Google Patents

Propulsive nozzle system Download PDF

Info

Publication number
EP0128337A3
EP0128337A3 EP84105051A EP84105051A EP0128337A3 EP 0128337 A3 EP0128337 A3 EP 0128337A3 EP 84105051 A EP84105051 A EP 84105051A EP 84105051 A EP84105051 A EP 84105051A EP 0128337 A3 EP0128337 A3 EP 0128337A3
Authority
EP
European Patent Office
Prior art keywords
nozzle system
propulsive nozzle
propulsive
nozzle
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.)
Granted
Application number
EP84105051A
Other languages
German (de)
Other versions
EP0128337A2 (en
EP0128337B1 (en
Inventor
Walter Kranz
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 EP0128337A2 publication Critical patent/EP0128337A2/en
Publication of EP0128337A3 publication Critical patent/EP0128337A3/en
Application granted granted Critical
Publication of EP0128337B1 publication Critical patent/EP0128337B1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
EP84105051A 1983-05-13 1984-05-04 Propulsive nozzle system Expired EP0128337B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3317583 1983-05-13
DE3317583A DE3317583C2 (en) 1983-05-13 1983-05-13 Device with a nozzle arrangement supplied by a propellant source

Publications (3)

Publication Number Publication Date
EP0128337A2 EP0128337A2 (en) 1984-12-19
EP0128337A3 true EP0128337A3 (en) 1985-09-18
EP0128337B1 EP0128337B1 (en) 1988-01-07

Family

ID=6198975

Family Applications (1)

Application Number Title Priority Date Filing Date
EP84105051A Expired EP0128337B1 (en) 1983-05-13 1984-05-04 Propulsive nozzle system

Country Status (4)

Country Link
US (1) US4589594A (en)
EP (1) EP0128337B1 (en)
DE (1) DE3317583C2 (en)
FR (1) FR2545879B1 (en)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3332415A1 (en) * 1983-09-08 1985-03-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn CONTROLLABLE FLOW DIVERSION SYSTEM
GB8417706D0 (en) * 1984-07-11 1994-01-26 British Aerospace Spin rate variation of spinning bodies
DE3429798C1 (en) * 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for correcting the trajectory of a projectile
DE3442975C2 (en) * 1984-11-24 1986-11-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for short-term control of a missile with the help of transverse force thrusters
DE3518904C1 (en) * 1985-05-25 1986-06-26 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Reversing motor
DE3519892A1 (en) * 1985-06-04 1986-12-04 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn BRAKE AND RELEASE DEVICE FOR A TURNTING BODY
DE3537079C1 (en) * 1985-10-18 1987-02-19 Messerschmitt Boelkow Blohm Quick-acting fluid control valve esp. for supersonic aircraft - has piston actuated by gas to deflect retaining balls
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
DE3606423A1 (en) * 1986-02-27 1987-09-03 Messerschmitt Boelkow Blohm ROTOR SYSTEM IN CONNECTION WITH AIRCRAFT CONTROLS
GB8604912D0 (en) * 1986-02-27 2007-04-04 Short Brothers Plc Flight control of missiles
GB8618510D0 (en) * 1986-07-29 1986-12-17 Imi Kynuch Ltd Guidance apparatus for projectiles
US5024395A (en) * 1987-01-27 1991-06-18 Messerschmitt Bolkow-Blohm Gmbh Stepping mechanism for rotary motions
DE3702240C1 (en) * 1987-01-27 1988-07-21 Messerschmitt Boelkow Blohm Actuating device for a rotating-nozzle arrangement for controlling missiles
DE3708312A1 (en) * 1987-03-14 1988-09-22 Messerschmitt Boelkow Blohm DEVICE FOR CONTROLLING AN AIRBODY
DE3742836C1 (en) * 1987-12-17 1989-07-13 Messerschmitt Boelkow Blohm Missile with adjustable control elements
DE3818615C1 (en) * 1988-06-01 1989-12-14 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Device for controlling missiles
FR2634548B1 (en) * 1988-07-22 1993-09-03 Thomson Brandt Armements
DE3838100A1 (en) * 1988-11-10 1990-05-17 Messerschmitt Boelkow Blohm FLUID DISTRIBUTOR
US5129604A (en) * 1989-07-17 1992-07-14 General Dynamics Corporation, Pomona Div. Lateral thrust assembly for missiles
DE4107054C2 (en) * 1991-03-06 1995-01-12 Rheinmetall Gmbh Trajectory correction device for ammunition
DE4408085C2 (en) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Device for guiding a missile not rotating about its longitudinal axis
US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6494140B1 (en) 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
US8186145B2 (en) * 2008-02-26 2012-05-29 Aerojet-General Corporation Rocket nozzles for unconventional vehicles
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
US9018572B2 (en) * 2012-11-06 2015-04-28 Raytheon Company Rocket propelled payload with divert control system within nose cone
RU2579294C1 (en) * 2015-06-16 2016-04-10 Акционерное общество "Конструкторское бюро химавтоматики" Liquid rocket engine with baffle at nozzle section
RU2657400C1 (en) * 2017-07-10 2018-06-13 Акционерное общество "Конструкторское бюро химавтоматики" Liquid rocket engine with a nozzle of carbon-carbon composite material (cccm)
IL271483A (en) * 2019-12-16 2021-06-30 Shilat Optronics Ltd Precision guided low-cost munitions system background

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3614027A (en) * 1969-07-08 1971-10-19 Us Army Pneumatic resolver for missile control
US3749334A (en) * 1966-04-04 1973-07-31 Us Army Attitude compensating missile system
FR2386802A1 (en) * 1977-04-08 1978-11-03 Thomson Brandt CONTROL DEVICE FOR PROJECTILE OF THE MISSILE GENUS, AND PROJECTILE EQUIPPED WITH THIS DEVICE
US4193567A (en) * 1962-07-17 1980-03-18 Novatronics, Inc. Guidance devices

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125297A (en) * 1964-03-17 Rotary spray head
DE2809281C2 (en) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Control device for a self-rotating projectile
GB2094240B (en) * 1981-03-10 1984-08-01 Secr Defence Attitude control systems for rocket powered vehicles
FR2504085A1 (en) * 1981-04-21 1982-10-22 Thomson Brandt DEVICE FOR STEAMING BY GAS JETS AND PROJECTILE COMPRISING SUCH A DEVICE
FR2504252B1 (en) * 1981-04-21 1987-03-06 Thomson Brandt PROJECTILE GUIDE
FR2508414B1 (en) * 1981-06-30 1985-06-07 Thomson Brandt GAS JET STEERING DEVICE FOR A GUIDED MACHINE

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193567A (en) * 1962-07-17 1980-03-18 Novatronics, Inc. Guidance devices
US3749334A (en) * 1966-04-04 1973-07-31 Us Army Attitude compensating missile system
US3614027A (en) * 1969-07-08 1971-10-19 Us Army Pneumatic resolver for missile control
FR2386802A1 (en) * 1977-04-08 1978-11-03 Thomson Brandt CONTROL DEVICE FOR PROJECTILE OF THE MISSILE GENUS, AND PROJECTILE EQUIPPED WITH THIS DEVICE

Also Published As

Publication number Publication date
US4589594A (en) 1986-05-20
EP0128337A2 (en) 1984-12-19
EP0128337B1 (en) 1988-01-07
DE3317583C2 (en) 1986-01-23
DE3317583A1 (en) 1984-11-29
FR2545879B1 (en) 1989-01-20
FR2545879A1 (en) 1984-11-16

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