GB982440A - Rocket propelled missile - Google Patents

Rocket propelled missile

Info

Publication number
GB982440A
GB982440A GB24209/57A GB2420957A GB982440A GB 982440 A GB982440 A GB 982440A GB 24209/57 A GB24209/57 A GB 24209/57A GB 2420957 A GB2420957 A GB 2420957A GB 982440 A GB982440 A GB 982440A
Authority
GB
United Kingdom
Prior art keywords
missile
stage
july
propelled missile
rocket propelled
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
GB24209/57A
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.)
De Havilland Aircraft of Canada Ltd
Original Assignee
De Havilland Aircraft of Canada 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 De Havilland Aircraft of Canada Ltd filed Critical De Havilland Aircraft of Canada Ltd
Publication of GB982440A publication Critical patent/GB982440A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
    • 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
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • 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

Landscapes

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

Abstract

982,440. Jet propulsion plant. DE HAVILLAND AIRCRAFT OF CANADA Ltd. July 30, 1957 [July 30, 1956], No. 24209/57. Heading F1J. [Also in Division F3] In a self-propelled missile, a first stage coaxially encloses a second stage rocket. The hot gases from the first stage pass rearwardly to an annular nozzle 32 containing deflector vanes 33 which impart spin to the missile.
GB24209/57A 1956-07-30 1957-07-30 Rocket propelled missile Expired GB982440A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US600859A US3167016A (en) 1956-07-30 1956-07-30 Rocket propelled missile

Publications (1)

Publication Number Publication Date
GB982440A true GB982440A (en) 1965-02-03

Family

ID=24405343

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24209/57A Expired GB982440A (en) 1956-07-30 1957-07-30 Rocket propelled missile

Country Status (2)

Country Link
US (1) US3167016A (en)
GB (1) GB982440A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1298369B (en) * 1966-07-30 1969-06-26 Messerschmitt Boelkow Blohm Multi-stage solid rocket
FR2482665A1 (en) * 1980-05-13 1981-11-20 Nissan Motor SOLID AND VARIABLE PUSH FUEL MOTOR

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377952A (en) * 1966-10-19 1968-04-16 Sydney R. Crockett Probe ejecting rocket motor
US3491692A (en) * 1967-02-18 1970-01-27 Bolkow Gmbh Multi-stage rocket
US3509821A (en) * 1969-01-06 1970-05-05 Stirling A Colgate Apparatus for accelerating rod-like objects
US3721196A (en) * 1970-07-30 1973-03-20 Us Navy Chaff dispensing system
EP0228781B1 (en) * 1985-10-31 1992-08-05 British Aerospace Public Limited Company Missile expulsion motor
US4964339A (en) * 1987-12-23 1990-10-23 General Dynamics Corp., Pomona Division Multiple stage rocket propelled missile system
US5005781A (en) * 1989-03-27 1991-04-09 Hughes Aircraft Company In-flight reconfigurable missile construction
US5020436A (en) * 1989-07-24 1991-06-04 General Dynamics Corp., Air Defense Systems Div. Booster retarding apparatus
US6058846A (en) * 1998-06-03 2000-05-09 Lockhead Martin Corporation Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section
US6584882B2 (en) * 2001-01-22 2003-07-01 Lockheed Martin Corporation Self-contained canister missile launcher with tubular exhaust uptake ducts
US20040041059A1 (en) * 2002-09-03 2004-03-04 Kennedy Kevin D. Device for projectile control
CN102089615B (en) * 2008-06-02 2014-01-29 考斯威夫公司 Projectile propulsion system
WO2010062780A2 (en) * 2008-11-03 2010-06-03 Causwave Electrical power generation
US8378509B2 (en) * 2009-11-03 2013-02-19 Causwave, Inc. Multiphase material generator vehicle
US10577129B1 (en) * 2015-05-19 2020-03-03 Peter Davis Poulsen Apparatus and methods for launching a payload
RU2629048C1 (en) * 2016-09-12 2017-08-24 Публичное акционерное общество "Научно-производственное объединение "Искра" Rocket and solid-propellant rocket engine
US11732677B2 (en) * 2021-02-22 2023-08-22 Raytheon Company Ring-shaped booster rocket
US11852103B2 (en) * 2021-02-22 2023-12-26 Raytheon Company Ring-shaped booster rocket

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US562535A (en) * 1896-06-23 Harris p
US1102653A (en) * 1913-10-01 1914-07-07 Robert H Goddard Rocket apparatus.
US2091635A (en) * 1934-09-24 1937-08-31 Kenneth L Hayden Projectile
FR816083A (en) * 1936-03-30 1937-07-29 Projectile improvements
US2611317A (en) * 1946-03-08 1952-09-23 Africano Alfred Rotating nozzle for rockets
US2478774A (en) * 1947-01-20 1949-08-09 Aden B Meinel Rocket launching device
FR1011653A (en) * 1949-02-25 1952-06-25 S E R A M Rocket launching and stabilizing devices
US2686473A (en) * 1949-05-11 1954-08-17 William F Vogel Missile
US2818779A (en) * 1952-04-24 1958-01-07 Casper J Koeper Non-tip off launcher

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1298369B (en) * 1966-07-30 1969-06-26 Messerschmitt Boelkow Blohm Multi-stage solid rocket
FR2482665A1 (en) * 1980-05-13 1981-11-20 Nissan Motor SOLID AND VARIABLE PUSH FUEL MOTOR

Also Published As

Publication number Publication date
US3167016A (en) 1965-01-26

Similar Documents

Publication Publication Date Title
GB982440A (en) Rocket propelled missile
GB884128A (en) Improvements in or relating to flying bodies for supersonic speeds
GB900040A (en) Exhaust nozzle with thrust deflector
GB627634A (en) Improvements in or relating to gas turbine aircraft propulsion power plants
GB907741A (en) Improvements relating to rockets
GB922876A (en) Jet-propelled aircraft with vertical take-off means
GB914598A (en) Aircraft control systems
GB697721A (en) Improvements in or relating to flying bodies
GB881663A (en) Improvements in or relating to gas turbine propulsion units
GB855591A (en) Arrangement of rocket drive mechanisms on flying objects
GB588085A (en) Improvements relating to propulsive thrust augmentors
GB756135A (en) Improvements in missile carrying aircraft
GB961842A (en) Improvements in or relating to aircraft having gas turbine jet propulsion engines
GB951969A (en) Improvements in and relating to a gyratory self-propelled projectile
GB832849A (en) Improvements in or relating to vehicle ejection seats
GB1024279A (en) Thrust chamber
CA531826A (en) Fuels for jet propelled aircraft
CA531549A (en) Rocket type jet propulsion units
CA531548A (en) Rocket type jet propulsion units
GB794768A (en) Jet propelling unit
CA555419A (en) Variable nozzles for gas-turbine reaction propulsion engines
MORDELL et al. Analysis of diffuser, combustor and nozzle design problems of hypersonic ramjets using supersonic combustion indicates high propulsion efficiencies up to mach 20
CA653306A (en) Gas turbine jet propulsion engine units for aircraft and also jet propelled aircraft
GB842971A (en) Directional control means for supersonic vehicle
AU217279B2 (en) Jet propulsion plant