DE2730751C2 - Flugkörper mit einem zylindrischen Rumpf - Google Patents

Flugkörper mit einem zylindrischen Rumpf

Info

Publication number
DE2730751C2
DE2730751C2 DE2730751A DE2730751A DE2730751C2 DE 2730751 C2 DE2730751 C2 DE 2730751C2 DE 2730751 A DE2730751 A DE 2730751A DE 2730751 A DE2730751 A DE 2730751A DE 2730751 C2 DE2730751 C2 DE 2730751C2
Authority
DE
Germany
Prior art keywords
missile
rudder
control
thrust
recoil
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
DE2730751A
Other languages
German (de)
English (en)
Other versions
DE2730751A1 (de
Inventor
Inge Claremont Calif. Maudal
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.)
Hughes Missile Systems Co (a Delaware Corp) Can
Original Assignee
General Dynamics Corp St Louis Mo
General Dynamics Corp
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
Priority to US05/603,218 priority Critical patent/US4044970A/en
Priority to GB25279/77A priority patent/GB1541528A/en
Priority to AU26286/77A priority patent/AU503846B2/en
Priority to NLAANVRAGE7707252,A priority patent/NL170890C/xx
Application filed by General Dynamics Corp St Louis Mo, General Dynamics Corp filed Critical General Dynamics Corp St Louis Mo
Priority to DE2730751A priority patent/DE2730751C2/de
Priority to BE1008266A priority patent/BE856661A/xx
Priority to FR7721144A priority patent/FR2396947A1/fr
Publication of DE2730751A1 publication Critical patent/DE2730751A1/de
Application granted granted Critical
Publication of DE2730751C2 publication Critical patent/DE2730751C2/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
    • 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
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins
    • 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • 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
    • 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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
DE2730751A 1975-08-08 1977-07-05 Flugkörper mit einem zylindrischen Rumpf Expired DE2730751C2 (de)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US05/603,218 US4044970A (en) 1975-08-08 1975-08-08 Integrated thrust vector aerodynamic control surface
GB25279/77A GB1541528A (en) 1975-08-08 1977-06-16 Integrated thrust vector aerodynamic control system for missible control and propulsion
AU26286/77A AU503846B2 (en) 1975-08-08 1977-06-21 Missile flight control
NLAANVRAGE7707252,A NL170890C (nl) 1975-08-08 1977-06-29 Geleid projectiel met inrichting voor het aanvullen van de stuwkracht van aerodynamische stuurvinnen.
DE2730751A DE2730751C2 (de) 1975-08-08 1977-07-05 Flugkörper mit einem zylindrischen Rumpf
BE1008266A BE856661A (fr) 1975-08-08 1977-07-08 Surface de guidage aerodynamique a vecteur poussee integre
FR7721144A FR2396947A1 (fr) 1975-08-08 1977-07-08 Surface de guidage aerodynamique a vecteur poussee integre

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
US05/603,218 US4044970A (en) 1975-08-08 1975-08-08 Integrated thrust vector aerodynamic control surface
GB25279/77A GB1541528A (en) 1975-08-08 1977-06-16 Integrated thrust vector aerodynamic control system for missible control and propulsion
AU26286/77A AU503846B2 (en) 1975-08-08 1977-06-21 Missile flight control
NLAANVRAGE7707252,A NL170890C (nl) 1975-08-08 1977-06-29 Geleid projectiel met inrichting voor het aanvullen van de stuwkracht van aerodynamische stuurvinnen.
DE2730751A DE2730751C2 (de) 1975-08-08 1977-07-05 Flugkörper mit einem zylindrischen Rumpf
BE1008266A BE856661A (fr) 1975-08-08 1977-07-08 Surface de guidage aerodynamique a vecteur poussee integre
FR7721144A FR2396947A1 (fr) 1975-08-08 1977-07-08 Surface de guidage aerodynamique a vecteur poussee integre
BE856661 1977-07-08

Publications (2)

Publication Number Publication Date
DE2730751A1 DE2730751A1 (de) 1979-01-18
DE2730751C2 true DE2730751C2 (de) 1984-02-23

Family

ID=37708370

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2730751A Expired DE2730751C2 (de) 1975-08-08 1977-07-05 Flugkörper mit einem zylindrischen Rumpf

Country Status (7)

Country Link
US (1) US4044970A (OSRAM)
AU (1) AU503846B2 (OSRAM)
BE (1) BE856661A (OSRAM)
DE (1) DE2730751C2 (OSRAM)
FR (1) FR2396947A1 (OSRAM)
GB (1) GB1541528A (OSRAM)
NL (1) NL170890C (OSRAM)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
US4272040A (en) * 1978-07-14 1981-06-09 General Dynamics, Pomona Division Aerodynamic control mechanism for thrust vector control
IL79864A (en) * 1985-11-25 1994-05-30 Hughes Aircraft Co Detachable vector thrust mechanism for an aeronautical vehicle
US4844380A (en) * 1985-11-25 1989-07-04 Hughes Aircraft Company Detachable thrust vector mechanism for an aeronautical vehicle
US4913379A (en) * 1988-02-23 1990-04-03 Japan as represented by Director General, Technical Research and Development Institute, Japan Defence Agency Rocket flight direction control system
US4867393A (en) * 1988-08-17 1989-09-19 Morton Thiokol, Inc. Reduced fin span thrust vector controlled pulsed tactical missile
WO1994010527A1 (fr) * 1992-10-23 1994-05-11 Arkhangelsky Ivan I Procede de guidage d'un missile et son dispositif de mise en ×uvre
US6224180B1 (en) 1997-02-21 2001-05-01 Gerald Pham-Van-Diep High speed jet soldering system
US8071926B2 (en) * 2009-01-13 2011-12-06 Simmonds Precision Products, Inc. Stability multiplexed autopilot
FR2970702B1 (fr) * 2011-01-26 2013-05-10 Astrium Sas Procede et systeme de pilotage d'un engin volant a propulseur arriere
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
RU2581787C2 (ru) * 2014-01-22 2016-04-20 Виктор Андреевич Павлов Способ стабилизации слабодемпфированного неустойчивого объекта управления и устройство для его осуществления
DE102020001703A1 (de) * 2020-03-14 2021-09-16 Diehl Defence Gmbh & Co. Kg Flugkörper, Flugzeug mit dem Flugkörper sowie Verfahren zum Abwerfen eines Flugkörpers aus einem Flugzeug
WO2021234355A1 (en) * 2020-05-21 2021-11-25 Mbda Uk Limited A missile servo actuation system and method of controlling a servo actuation system in a missile
US12151810B2 (en) 2020-09-30 2024-11-26 Zhejiang University Tailstock type vertical take-off and landing unmanned aerial vehicle and control method thereof
CN112158325B (zh) * 2020-09-30 2022-02-18 浙江大学 一种尾座式垂直起降无人机及其控制方法
CN116772663B (zh) * 2023-07-13 2025-11-18 北京理工大学 一种导弹的敏捷转弯控制方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013494A (en) * 1957-08-09 1961-12-19 Chanut Pierre Louis Jean Guided missile
US3164338A (en) * 1959-06-29 1965-01-05 Gen Electric Atmosphere re-entry system for spacecraft
US3276376A (en) * 1964-09-30 1966-10-04 Robert W Cubbison Thrust and direction control apparatus
US3286956A (en) * 1965-07-19 1966-11-22 Douglas Aircraft Co Inc Missile control system

Also Published As

Publication number Publication date
FR2396947A1 (fr) 1979-02-02
FR2396947B1 (OSRAM) 1981-10-23
GB1541528A (en) 1979-03-07
AU503846B2 (en) 1979-09-20
BE856661A (fr) 1978-01-09
AU2628677A (en) 1979-01-04
NL7707252A (nl) 1979-01-03
NL170890C (nl) 1983-01-03
US4044970A (en) 1977-08-30
DE2730751A1 (de) 1979-01-18
NL170890B (nl) 1982-08-02

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Legal Events

Date Code Title Description
OAP Request for examination filed
OD Request for examination
D2 Grant after examination
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: HUGHES MISSILE SYSTEMS CO. (A DELAWARE CORP.), CAN

8328 Change in the person/name/address of the agent

Free format text: RUSCHKE, H., DIPL.-ING., 81679 MUENCHEN RUSCHKE, O., DIPL.-ING., PAT.-ANWAELTE, 10707 BERLIN

8339 Ceased/non-payment of the annual fee