DE1132029C2 - - Google Patents

Info

Publication number
DE1132029C2
DE1132029C2 DE1959I0017424 DEI0017424A DE1132029C2 DE 1132029 C2 DE1132029 C2 DE 1132029C2 DE 1959I0017424 DE1959I0017424 DE 1959I0017424 DE I0017424 A DEI0017424 A DE I0017424A DE 1132029 C2 DE1132029 C2 DE 1132029C2
Authority
DE
Germany
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
DE1959I0017424
Other languages
German (de)
Other versions
DE1132029B (de
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 filed Critical
Publication of DE1132029B publication Critical patent/DE1132029B/de
Application granted granted Critical
Publication of DE1132029C2 publication Critical patent/DE1132029C2/de
Granted 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Transmission Devices (AREA)
DEI17424A 1958-12-31 1959-12-21 Steuervorrichtung fuer Raketen Granted DE1132029B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB42271/58A GB875205A (en) 1958-12-31 1958-12-31 Improvements relating to rocket propulsion

Publications (2)

Publication Number Publication Date
DE1132029B DE1132029B (de) 1962-06-20
DE1132029C2 true DE1132029C2 (h) 1962-12-27

Family

ID=10423674

Family Applications (1)

Application Number Title Priority Date Filing Date
DEI17424A Granted DE1132029B (de) 1958-12-31 1959-12-21 Steuervorrichtung fuer Raketen

Country Status (3)

Country Link
BE (1) BE602973A (h)
DE (1) DE1132029B (h)
GB (1) GB875205A (h)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1332562A (fr) * 1962-03-20 1963-07-19 Snecma Dispositif de tourillonnement et d'étanchéité pour tuyère, applicable notamment aux fusées
US3235184A (en) * 1963-03-20 1966-02-15 Curtiss Wright Corp Vectoring nozzle
FR1376511A (fr) * 1963-05-06 1964-10-31 Snecma Propulseur à réaction à tuyère mobile
US3362646A (en) * 1965-08-23 1968-01-09 Thiokol Chemical Corp Variable direction thrust nozzle
US4432512A (en) * 1978-08-31 1984-02-21 British Aerospace Public Limited Company Jet propulsion efflux outlets
DE3003231C2 (de) * 1980-01-30 1984-01-05 Dornier Gmbh, 7990 Friedrichshafen Steuereinrichtung für durch Strahlreaktion angetriebene Flugkörper, Raketen o.dgl.
EP3330189B1 (en) 2016-12-05 2019-06-19 Airbus Defence and Space GmbH Pointing mechanism for use in an electric propulsion system of a spacecraft
CN115898701A (zh) * 2022-10-28 2023-04-04 西安航天发动机有限公司 一种用于推力室头部的组合自紧式密封结构

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH196692A (fr) * 1936-12-31 1938-03-31 Sageb Societe Anonyme De Gesti Projectile comportant une fusée à réaction.
US2611317A (en) * 1946-03-08 1952-09-23 Africano Alfred Rotating nozzle for rockets
US2849955A (en) * 1955-06-30 1958-09-02 Spurgeon E Smathers Rocket construction

Also Published As

Publication number Publication date
DE1132029B (de) 1962-06-20
GB875205A (en) 1961-08-16
BE602973A (fr) 1961-10-24

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