GB875205A - Improvements relating to rocket propulsion - Google Patents

Improvements relating to rocket propulsion

Info

Publication number
GB875205A
GB875205A GB42271/58A GB4227158A GB875205A GB 875205 A GB875205 A GB 875205A GB 42271/58 A GB42271/58 A GB 42271/58A GB 4227158 A GB4227158 A GB 4227158A GB 875205 A GB875205 A GB 875205A
Authority
GB
United Kingdom
Prior art keywords
nozzle
axis
nozzles
ring
symmetry
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
GB42271/58A
Other languages
English (en)
Inventor
John Michael Minden Carter
Frank Conwy Morgan
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.)
Imperial Chemical Industries Ltd
Original Assignee
Imperial Chemical Industries Ltd
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 Imperial Chemical Industries Ltd filed Critical Imperial Chemical Industries Ltd
Priority to GB42271/58A priority Critical patent/GB875205A/en
Priority to DEI17424A priority patent/DE1132029B/de
Priority to BE602973A priority patent/BE602973A/fr
Publication of GB875205A publication Critical patent/GB875205A/en
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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (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)
GB42271/58A 1958-12-31 1958-12-31 Improvements relating to rocket propulsion Expired GB875205A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB42271/58A GB875205A (en) 1958-12-31 1958-12-31 Improvements relating to rocket propulsion
DEI17424A DE1132029B (de) 1958-12-31 1959-12-21 Steuervorrichtung fuer Raketen
BE602973A BE602973A (fr) 1958-12-31 1961-04-24 Perfectionnements à la propulsion par fusées.

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 (1)

Publication Number Publication Date
GB875205A true GB875205A (en) 1961-08-16

Family

ID=10423674

Family Applications (1)

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

Country Status (3)

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

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3159969A (en) * 1962-03-20 1964-12-08 Snecma Sealing and rotatable mounting arrangement for rocket nozzles
US3235184A (en) * 1963-03-20 1966-02-15 Curtiss Wright Corp Vectoring nozzle
US3362646A (en) * 1965-08-23 1968-01-09 Thiokol Chemical Corp Variable direction thrust nozzle
FR2474439A1 (fr) * 1980-01-30 1981-07-31 Dornier Gmbh Dispositif de commande pour engins de navigation aerienne, fusees, etc., mus par reacteurs
US4432512A (en) * 1978-08-31 1984-02-21 British Aerospace Public Limited Company Jet propulsion efflux outlets
EP3330189A1 (fr) * 2016-12-05 2018-06-06 Airbus Defence and Space GmbH Mécanisme de pointage destiné à être utilisé dans un système de propulsion électrique d'un engin spatial
WO2024087811A1 (fr) * 2022-10-28 2024-05-02 西安航天发动机有限公司 Structure d'étanchéité combinée à auto-serrage pour tête de chambre de poussée

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

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3159969A (en) * 1962-03-20 1964-12-08 Snecma Sealing and rotatable mounting arrangement for rocket nozzles
US3235184A (en) * 1963-03-20 1966-02-15 Curtiss Wright Corp Vectoring nozzle
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
FR2474439A1 (fr) * 1980-01-30 1981-07-31 Dornier Gmbh Dispositif de commande pour engins de navigation aerienne, fusees, etc., mus par reacteurs
EP3330189A1 (fr) * 2016-12-05 2018-06-06 Airbus Defence and Space GmbH Mécanisme de pointage destiné à être utilisé dans un système de propulsion électrique d'un engin spatial
US10737807B2 (en) 2016-12-05 2020-08-11 Airbus Defence and Space GmbH Pointing mechanism for use in an electric propulsion system of a spacecraft and electric propulsion system for use in a spacecraft
WO2024087811A1 (fr) * 2022-10-28 2024-05-02 西安航天发动机有限公司 Structure d'étanchéité combinée à auto-serrage pour tête de chambre de poussée

Also Published As

Publication number Publication date
DE1132029C2 (fr) 1962-12-27
DE1132029B (de) 1962-06-20
BE602973A (fr) 1961-10-24

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