BE592129A - Perfectionnements aux fusées - Google Patents

Perfectionnements aux fusées

Info

Publication number
BE592129A
BE592129A BE592129A BE592129A BE592129A BE 592129 A BE592129 A BE 592129A BE 592129 A BE592129 A BE 592129A BE 592129 A BE592129 A BE 592129A BE 592129 A BE592129 A BE 592129A
Authority
BE
Belgium
Prior art keywords
rocket
refinements
rocket refinements
Prior art date
Application number
BE592129A
Other languages
English (en)
Inventor
Julius W Tumavicus
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of BE592129A publication Critical patent/BE592129A/fr

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
    • 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

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)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)
  • Automatic Assembly (AREA)
  • Transmission Devices (AREA)
BE592129A 1959-06-25 1960-06-21 Perfectionnements aux fusées BE592129A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US822885A US3057581A (en) 1959-06-25 1959-06-25 Rocket vectoring arrangement

Publications (1)

Publication Number Publication Date
BE592129A true BE592129A (fr) 1960-10-17

Family

ID=25237236

Family Applications (1)

Application Number Title Priority Date Filing Date
BE592129A BE592129A (fr) 1959-06-25 1960-06-21 Perfectionnements aux fusées

Country Status (5)

Country Link
US (1) US3057581A (fr)
BE (1) BE592129A (fr)
CH (1) CH381020A (fr)
DE (1) DE1428720A1 (fr)
GB (1) GB892246A (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279183A (en) * 1962-09-07 1966-10-18 United Aircraft Corp Vectorable plug cluster nozzle rocket
US3314609A (en) * 1962-09-07 1967-04-18 United Aircraft Corp Vectorable plug cluster nozzle rocket
US3304721A (en) * 1964-09-08 1967-02-21 George U Oppel Aircraft thrust vector control assembly
US3604628A (en) * 1969-08-01 1971-09-14 United Aircraft Corp Skewed exit plane nozzle system for optimum thrust
US3667567A (en) * 1970-02-26 1972-06-06 Trw Inc Rocket powered ground effect machine
US4327885A (en) * 1971-10-06 1982-05-04 The United States Of America As Represented By The Secretary Of The Navy Thrust augmented rocket
DE2721656A1 (de) * 1977-05-13 1978-11-16 Ver Flugtechnische Werke Stellanordnung zur steuerung von flugkoerpern
DE3003231C2 (de) * 1980-01-30 1984-01-05 Dornier Gmbh, 7990 Friedrichshafen Steuereinrichtung für durch Strahlreaktion angetriebene Flugkörper, Raketen o.dgl.
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
US4967982A (en) * 1988-11-07 1990-11-06 General Dynamics Corp., Pomona Division Lateral thruster for missiles
US7407133B2 (en) * 2001-07-24 2008-08-05 3X Jet Aircraft Company Using imbalanced thrust in a multi-engine jet aircraft
US8002219B2 (en) * 2006-11-17 2011-08-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Multi-functional annular fairing for coupling launch abort motor to space vehicle
US8975565B2 (en) * 2012-07-17 2015-03-10 Raytheon Company Integrated propulsion and attitude control system from a common pressure vessel for an interceptor
US8998131B1 (en) * 2013-10-17 2015-04-07 The Boeing Company Differential throttling control enhancement
GB201916363D0 (en) * 2019-11-11 2019-12-25 Mbda Uk Ltd Exhaust nozzle assembly
DE102022003287A1 (de) * 2022-09-07 2024-03-07 Diehl Defence Gmbh & Co. Kg Lenkflugkörper

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422744A (en) * 1944-09-30 1947-06-24 Gen Tire & Rubber Co Auxiliary jet power means for aircraft
FR1040930A (fr) * 1951-07-24 1953-10-20 Aérodyne perfectionné
US2938459A (en) * 1956-05-11 1960-05-31 North American Aviation Inc Cross-bearing gimbal

Also Published As

Publication number Publication date
DE1428720A1 (de) 1969-01-23
US3057581A (en) 1962-10-09
GB892246A (en) 1962-03-21
CH381020A (de) 1964-08-15

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