GB696751A - Improvements in or relating to flying bodies - Google Patents

Improvements in or relating to flying bodies

Info

Publication number
GB696751A
GB696751A GB203249A GB203249A GB696751A GB 696751 A GB696751 A GB 696751A GB 203249 A GB203249 A GB 203249A GB 203249 A GB203249 A GB 203249A GB 696751 A GB696751 A GB 696751A
Authority
GB
United Kingdom
Prior art keywords
rockets
noses
sleeve
band
tails
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
GB203249A
Inventor
Leslie Woodhouse Reeve
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB203249A priority Critical patent/GB696751A/en
Publication of GB696751A publication Critical patent/GB696751A/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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

696,751. Releasing starting rockets. FAIREY AVIATION CO., Ltd. Jan. 19. 1950 [Jan. 25, 1949], No. 2032/49. Class 9(ii) [Also in Group XXXIII] Starting rockets 14 around a missile 10 are secured by the noses and tails, the noses by the lugs 18 fitting over the spigots 19 on the band 20, and the tails by the band 28 which is affixed by the arms 29 to the segmented collar 33 and 34. Before launching, the piston 22 in the sleeve 21 of the lug 18 isfreed, so that, on the rockets firing, the sleeve 21 moves towards the band 20 to compress the spring 24. When the thrust of the rockets falls below the pressure of the spring 24, the sleeve 21 comes away from the spigot 19 and the released noses are swung outwards because of the air pressure on the vanes 17. The arms 29 pivot about the pin 31 causing the pin 38 to be withdrawn by the claws 32 and allowing a part of the sectional collar to fall away with its associated rocket.
GB203249A 1949-01-25 1949-01-25 Improvements in or relating to flying bodies Expired GB696751A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB203249A GB696751A (en) 1949-01-25 1949-01-25 Improvements in or relating to flying bodies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB203249A GB696751A (en) 1949-01-25 1949-01-25 Improvements in or relating to flying bodies

Publications (1)

Publication Number Publication Date
GB696751A true GB696751A (en) 1953-09-09

Family

ID=9732409

Family Applications (1)

Application Number Title Priority Date Filing Date
GB203249A Expired GB696751A (en) 1949-01-25 1949-01-25 Improvements in or relating to flying bodies

Country Status (1)

Country Link
GB (1) GB696751A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
US3369771A (en) * 1964-06-18 1968-02-20 British Aircraft Corp Ltd Space vehicles
EP0466580A1 (en) * 1990-07-11 1992-01-15 AEROSPATIALE Société Nationale Industrielle Forward end structure of a rocket booster mounted on the main body of a launcher
US20150048212A1 (en) * 2013-08-19 2015-02-19 The Boeing Company Unsteady aerodynamics mitigation for multi-body aerospace apparatus
CN107976123A (en) * 2017-11-14 2018-05-01 南京理工大学 A kind of shrapnel inertia kinetic energy formula scattering mechanism

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
US3369771A (en) * 1964-06-18 1968-02-20 British Aircraft Corp Ltd Space vehicles
EP0466580A1 (en) * 1990-07-11 1992-01-15 AEROSPATIALE Société Nationale Industrielle Forward end structure of a rocket booster mounted on the main body of a launcher
FR2664563A1 (en) * 1990-07-11 1992-01-17 Aerospatiale FRONT END STRUCTURE OF A BOOSTER PROPELLER MOUNTED ON THE MAIN BODY OF A LAUNCHER.
US5131610A (en) * 1990-07-11 1992-07-21 Aerospatiale Societe Nationale Industrielle Front end structure of a booster rocket mounted on the main body of a launcher
US20150048212A1 (en) * 2013-08-19 2015-02-19 The Boeing Company Unsteady aerodynamics mitigation for multi-body aerospace apparatus
CN107976123A (en) * 2017-11-14 2018-05-01 南京理工大学 A kind of shrapnel inertia kinetic energy formula scattering mechanism
CN107976123B (en) * 2017-11-14 2019-07-26 南京理工大学 A kind of shrapnel inertia kinetic energy formula scattering mechanism

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