GB855592A - Improvements in or relating to rocket missiles - Google Patents

Improvements in or relating to rocket missiles

Info

Publication number
GB855592A
GB855592A GB11080/57A GB1108057A GB855592A GB 855592 A GB855592 A GB 855592A GB 11080/57 A GB11080/57 A GB 11080/57A GB 1108057 A GB1108057 A GB 1108057A GB 855592 A GB855592 A GB 855592A
Authority
GB
United Kingdom
Prior art keywords
missile
charge
nozzle
fins
attached
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
GB11080/57A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB855592A publication Critical patent/GB855592A/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
    • 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
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins

Landscapes

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

Abstract

855,592. Self-propelled missiles. BOLKOW, L. April 4, 1957 [April 5, 1956], No. 11080/57. Class 9(2). A self-propelled missile 1 having a main propellant charge 8 and a launching charge 10 attached to the body 1 is provided with a discharge nozzle 9 for the gases from charge 10, which is arranged to give, when the missile is orientated with the nozzle 9 facing downwards, both an upward lift and a forward thrust, so that the missile may be launched directly from the ground. The missile, which contains a hollow charge, has a conically tapered nose and is provided with four mutually perpendicular fins 3 - 6, attached to the body 1 by means of feet 7. The nozzle 9 is inclined atan angle α > 15 degrees to the longitudinal axis of the projectile, so that the axis of the nozzle passes through the centre of gravity S which lies within the zone of the fins. Each fin may house steering devices 11, e.g. magnetic drives acting on adjustable control surfaces. The casing of charge 10 is attached at the forward end to the body 1 by a pin 15 engaged in bracket 13 and at the rear by solder 16, which is melted by the burning of charge 10. When charge 10 is burnt out, the casing falls away from the missile. To launch the missile, it is placed on the ground supported by two fins between which nozzle 9 is directed downwardly. To give additional support the forward end of the rocket may rest on a bracket, which is retracted by a spring when the missile leaves the ground.
GB11080/57A 1956-04-05 1957-04-04 Improvements in or relating to rocket missiles Expired GB855592A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB39751A DE1078903B (en) 1956-04-05 1956-04-05 Rocket propelled missile

Publications (1)

Publication Number Publication Date
GB855592A true GB855592A (en) 1960-12-07

Family

ID=6965894

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11080/57A Expired GB855592A (en) 1956-04-05 1957-04-04 Improvements in or relating to rocket missiles

Country Status (5)

Country Link
US (1) US2946285A (en)
CH (1) CH363908A (en)
DE (1) DE1078903B (en)
FR (1) FR1173322A (en)
GB (1) GB855592A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107933946A (en) * 2017-12-11 2018-04-20 浙江大学 Unmanned plane two point form rocket assist emitter and its method

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1125814B (en) * 1959-01-28 1962-03-15 Boelkow Entwicklungen Kg Protection device for sensitive parts on rocket propelled missiles
US3132827A (en) * 1960-08-27 1964-05-12 Onera (Off Nat Aerospatiale) High speed airplane having auxiliary rockets
US3403873A (en) * 1963-01-24 1968-10-01 Navy Usa Guided missile
US4445652A (en) * 1982-03-25 1984-05-01 The Boeing Company Adjustable rocket thrust alignment device
US4949918A (en) * 1989-08-02 1990-08-21 Arszman Jerrold H Moment control of rockets
CN111306994B (en) * 2020-05-07 2021-06-01 北京理工大学 Reusable composite material missile bracket

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE305160C (en) *
US1629767A (en) * 1924-03-18 1927-05-24 Valdes Salustio Jet-propulsion apparatus for the driving of vehicles, ships, boats, flying machines, and the like
US2503271A (en) * 1945-02-06 1950-04-11 Clarence N Hickman Rocket projectile
US2537487A (en) * 1946-03-01 1951-01-09 Stone William Card Adjustable exhaust for jetpropelled aircraft
US2596644A (en) * 1946-12-10 1952-05-13 Us Sec War Automatically detachable flashless nozzle for rockets
US2748703A (en) * 1948-04-27 1956-06-05 Wilbur H Goss Rocket type launching carriage for ordnance missile
US2787218A (en) * 1952-02-25 1957-04-02 Anthony Alastair Aircraft
US2818779A (en) * 1952-04-24 1958-01-07 Casper J Koeper Non-tip off launcher
US2833494A (en) * 1953-06-15 1958-05-06 Northrop Aircraft Inc Rocket ejection system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107933946A (en) * 2017-12-11 2018-04-20 浙江大学 Unmanned plane two point form rocket assist emitter and its method

Also Published As

Publication number Publication date
FR1173322A (en) 1959-02-24
DE1078903B (en) 1960-03-31
US2946285A (en) 1960-07-26
CH363908A (en) 1962-08-15

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