FR1365790A - Organe de direction pour fusées - Google Patents

Organe de direction pour fusées

Info

Publication number
FR1365790A
FR1365790A FR944162A FR944162A FR1365790A FR 1365790 A FR1365790 A FR 1365790A FR 944162 A FR944162 A FR 944162A FR 944162 A FR944162 A FR 944162A FR 1365790 A FR1365790 A FR 1365790A
Authority
FR
France
Prior art keywords
rockets
steering unit
steering
unit
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
FR944162A
Other languages
English (en)
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.)
ATK Launch Systems LLC
Original Assignee
Thiokol 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
Application filed by Thiokol Corp filed Critical Thiokol Corp
Application granted granted Critical
Publication of FR1365790A publication Critical patent/FR1365790A/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Special Conveying (AREA)
  • Testing Of Engines (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR944162A 1962-08-10 1963-08-08 Organe de direction pour fusées Expired FR1365790A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US216203A US3246468A (en) 1962-08-10 1962-08-10 Steering means for rockets

Publications (1)

Publication Number Publication Date
FR1365790A true FR1365790A (fr) 1964-07-03

Family

ID=22806152

Family Applications (1)

Application Number Title Priority Date Filing Date
FR944162A Expired FR1365790A (fr) 1962-08-10 1963-08-08 Organe de direction pour fusées

Country Status (4)

Country Link
US (1) US3246468A (fr)
DE (1) DE1220288B (fr)
FR (1) FR1365790A (fr)
GB (1) GB1045885A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2194883A1 (fr) * 1972-07-31 1974-03-01 Bofors Ab

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ198917A (en) * 1980-11-14 1985-01-31 Commw Of Australia Rocket controlled by spoiler tabs in exhaust
US5072891A (en) * 1989-11-22 1991-12-17 Applied Technology Associates Combination actuator and coolant supply for missile and rocket vector control
DE102008022289B4 (de) * 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1879187A (en) * 1931-02-07 1932-09-27 Robert H Goddard Mechanism for directing flight
CH316187A (fr) * 1951-08-02 1956-09-30 Zborowski Helmut Ph G A R Von Aérodyne
US2945344A (en) * 1956-10-23 1960-07-19 Phillips Petroleum Co Gas generator adapted for on-off operation
US3026806A (en) * 1957-03-22 1962-03-27 Russell Mfg Co Ballistic missile nose cone
US3036430A (en) * 1958-06-19 1962-05-29 Snecma Jet control apparatus
US3096049A (en) * 1960-01-25 1963-07-02 Edward S Karasinski Steering means for space vehicles missiles and high altitude flying craft
US3022190A (en) * 1960-02-15 1962-02-20 Emerson Electric Mfg Co Process of and composition for controlling temperatures

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2194883A1 (fr) * 1972-07-31 1974-03-01 Bofors Ab

Also Published As

Publication number Publication date
DE1220288B (de) 1966-06-30
US3246468A (en) 1966-04-19
GB1045885A (en) 1966-10-19
DE1220288C2 (fr) 1967-01-19

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