FR1504910A - Engin volant à commande de la trajectoire par vecteur de poussée - Google Patents

Engin volant à commande de la trajectoire par vecteur de poussée

Info

Publication number
FR1504910A
FR1504910A FR86359A FR86359A FR1504910A FR 1504910 A FR1504910 A FR 1504910A FR 86359 A FR86359 A FR 86359A FR 86359 A FR86359 A FR 86359A FR 1504910 A FR1504910 A FR 1504910A
Authority
FR
France
Prior art keywords
thrust vector
flying machine
machine controlled
flying
controlled
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
FR86359A
Other languages
English (en)
French (fr)
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.)
Bolkow GmbH
Original Assignee
Bolkow GmbH
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 Bolkow GmbH filed Critical Bolkow GmbH
Application granted granted Critical
Publication of FR1504910A publication Critical patent/FR1504910A/fr
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
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B64G1/262—Guiding or controlling apparatus, e.g. for attitude control using jets having adjustable angles, e.g. gimbaled thrusters
    • 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
    • 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
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • 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
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position Or Direction (AREA)
FR86359A 1965-12-10 1966-12-06 Engin volant à commande de la trajectoire par vecteur de poussée Expired FR1504910A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB84921A DE1298912B (de) 1965-12-10 1965-12-10 Schubvektorsteuerung fuer einen raketengetriebenen Flugkoerper mit mindestens einem Strahlablenker

Publications (1)

Publication Number Publication Date
FR1504910A true FR1504910A (fr) 1967-12-08

Family

ID=6982666

Family Applications (1)

Application Number Title Priority Date Filing Date
FR86359A Expired FR1504910A (fr) 1965-12-10 1966-12-06 Engin volant à commande de la trajectoire par vecteur de poussée

Country Status (6)

Country Link
US (1) US3384325A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CH (1) CH447831A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE1298912B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR1504910A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1158258A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
SE (1) SE331040B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2444805A1 (fr) * 1978-12-20 1980-07-18 Europ Propulsion Dispositif de deviation du jet d'une tuyere de propulseur-fusee

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO130026B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1969-08-12 1974-06-24 Imp Metal Ind Kynoch Ltd
US3986683A (en) * 1974-03-27 1976-10-19 The United States Of America As Represented By The Secretary Of The Air Force Jet tab steerable missile
SE408323B (sv) * 1976-06-08 1979-06-05 Bofors Ab Styranordning for en ballistisk enhet
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
GB8417706D0 (en) * 1984-07-11 1994-01-26 British Aerospace Spin rate variation of spinning bodies
FR2705773B1 (fr) * 1993-05-28 1995-08-04 Aerospatiale Système de pilotage d'un aéronef par interception du jet propulsif.
FR2706200B1 (fr) * 1993-06-07 1995-08-11 Aerospatiale Système d'actionnement pour gouverne aérodynamique et systèmes pour le pilotage d'aéronefs, comportant au moins un tel système d'actionnement.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2879955A (en) * 1951-08-02 1959-03-31 Zborowski Helmut P G A R Von Airborne bodies and in particular self propelled missiles
FR1040316A (fr) * 1951-08-02 1953-10-14 Perfectionnements apportés aux aérodynes, notamment aux projectiles auto-propulsés à charge creuse
US3010677A (en) * 1957-11-12 1961-11-28 Gen Dynamics Corp Missile control system
DE1109534B (de) * 1958-01-15 1961-06-22 Boelkow Entwicklungen Kg Verfahren und Vorrichtung zur Steuerung und Stabilisierung von Flugkoerpern
US3147591A (en) * 1961-12-28 1964-09-08 Gen Motors Corp Swiveling fluid jet exhaust nozzle construction
US3276376A (en) * 1964-09-30 1966-10-04 Robert W Cubbison Thrust and direction control apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2444805A1 (fr) * 1978-12-20 1980-07-18 Europ Propulsion Dispositif de deviation du jet d'une tuyere de propulseur-fusee

Also Published As

Publication number Publication date
SE331040B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1970-12-07
CH447831A (de) 1967-11-30
US3384325A (en) 1968-05-21
DE1298912B (de) 1969-07-03
GB1158258A (en) 1969-07-16

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