GB516818A - Improvements in or relating to projectiles comprising a reaction propulsion device - Google Patents

Improvements in or relating to projectiles comprising a reaction propulsion device

Info

Publication number
GB516818A
GB516818A GB18962/38A GB1896238A GB516818A GB 516818 A GB516818 A GB 516818A GB 18962/38 A GB18962/38 A GB 18962/38A GB 1896238 A GB1896238 A GB 1896238A GB 516818 A GB516818 A GB 516818A
Authority
GB
United Kingdom
Prior art keywords
charge
projectile
shell
projectiles
reaction
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
GB18962/38A
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.)
SAGEB SA
Original Assignee
SAGEB SA
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 SAGEB SA filed Critical SAGEB SA
Publication of GB516818A publication Critical patent/GB516818A/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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10—Shape or structure of solid propellant charges

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Plasma Technology (AREA)
  • Nozzles (AREA)
  • Ceramic Products (AREA)

Abstract

516,818. Projectiles; bombs. SAGEB SOC. ANON. DE GESTION ET D'EXPLOITATION DE BREVETS. June 27, 1938, No. 18962. Convention date, June 28, 1937. [Class 9 (i)] Relates to projectiles and bombs of the kind described in Specification 489,876, in which a reaction propulsion charge discharges through laterallydisposed nozzles on the periphery of the projectile. According to the invention, the projectile,. whether an artillery shell or aircraft bomb, has an outer casing of streamline form, inside which is carried near the centre of gravity of the whole projectile, the offensive charge in an armour - piercing or other shell body. Fig. 1 shows an artillery projectile having a stream - lined outer casing the front end @ of which has an inflected curvature, as described in Specification 507,107, and both the front and rear ends of which contain propulsive reaction charges which discharge, when ignited, through lateral nozzles 4, 5, respectively. The nozzles are provided in a ring 3 within which is mounted a 'shell 1 carrying the offensive charge 9. G indicates the centre of gravity of the whole projectile. The charge 9 may be exploded, on impact, by a percussion fuze 11 connected by a tube 12 to a detonator 13 in the shell 1. Driving bands 17, 18 are arranged as shown. Fig. 5 shows an aerial bomb in which the reaction jets 5 for the the charge 22 are located in front of the centre of gravity G, and in which the shell 30 containing the offensive charge is of bulbous form at 60. An ignition means for the reaction charge 22 is provided at 15. The Specification as open to inspection under Sect. 91 comprises also the subject-matter of Specifications 516,463 and 516,865. Other forms of projectiles and bombs are also described, including means for assembling a stream-lined projectile and a cartridge case by means of the rear driving band and a sealing band located in rear of the driving band. This subjectmatter does not appear in the Specification as accepted.
GB18962/38A 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion device Expired GB516818A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
LU208567X 1937-06-28

Publications (1)

Publication Number Publication Date
GB516818A true GB516818A (en) 1940-01-12

Family

ID=19732351

Family Applications (3)

Application Number Title Priority Date Filing Date
GB5020/39A Expired GB516865A (en) 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion devices
GB5019/39A Expired GB516463A (en) 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion device
GB18962/38A Expired GB516818A (en) 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion device

Family Applications Before (2)

Application Number Title Priority Date Filing Date
GB5020/39A Expired GB516865A (en) 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion devices
GB5019/39A Expired GB516463A (en) 1937-06-28 1938-06-27 Improvements in or relating to projectiles comprising a reaction propulsion device

Country Status (4)

Country Link
BE (1) BE428854A (en)
CH (1) CH208567A (en)
FR (1) FR839861A (en)
GB (3) GB516865A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479718A (en) * 1947-01-29 1949-08-23 Carold F Bjork Rocket projectile
US2503271A (en) * 1945-02-06 1950-04-11 Clarence N Hickman Rocket projectile
US2613605A (en) * 1946-11-09 1952-10-14 Energa Projectile
US2690314A (en) * 1949-12-15 1954-09-28 Us Navy Long-range guided athodyd
US2701525A (en) * 1952-04-03 1955-02-08 Clarence N Hickman Mortar shell loading driver rocket
US3144828A (en) * 1962-06-30 1964-08-18 Rheinmetall Gmbh Spin-stabilized rocket projectile
US3277825A (en) * 1963-11-07 1966-10-11 Brevets Aero Mecaniques Self-propelled armor-piercing shells
US3807275A (en) * 1972-10-06 1974-04-30 Us Army Miniature missile system
FR2412812A1 (en) * 1977-12-23 1979-07-20 Rheinmetall Gmbh DEVICE ALLOWING TO MODIFY THE TRAJECTORY OF A PROJECTILE

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB594516A (en) * 1940-09-04 1947-11-13 Charles Dennistoun Burney Improvements in or relating to projectiles operating with rocket propulsion
GB579807A (en) * 1941-02-11 1946-08-16 Walter Gordon Wilson Improvements in and relating to the propulsion of aerial torpedoes
US2446560A (en) * 1941-09-19 1948-08-10 Us Sec War Rocket charge suspension arrangement
US2504648A (en) * 1941-10-25 1950-04-18 Edward F Chandler Projectile
US2574479A (en) * 1943-01-30 1951-11-13 Clarence N Hickman Propellant having an opacifier for preventing self-ignition by radiant energy radiations
US2515048A (en) * 1943-04-02 1950-07-11 Us Navy Multiple rocket motor
US2440271A (en) * 1944-06-26 1948-04-27 Us Sec War Rocket projectile
US2500117A (en) * 1944-07-19 1950-03-07 Edward F Chandler Rocket projectile
US2712283A (en) * 1944-07-20 1955-07-05 Golden Sidney Propellent assembly for jet propelled device
US2422720A (en) * 1944-08-15 1947-06-24 Carolus L Eksergian Rocket projectile
US2548926A (en) * 1944-10-03 1951-04-17 Africano Alfred Insulated trap for rocket projectiles
US2422721A (en) * 1944-10-13 1947-06-24 William W Farr Rocket projectile
US2763127A (en) * 1945-01-27 1956-09-18 Golden Sidney Jet propelled device
US2510110A (en) * 1945-03-30 1950-06-06 Clarence N Hickman Step-motor rocket projectile
US2519905A (en) * 1945-05-17 1950-08-22 Clarence N Hickman Driver rocket
US2976804A (en) * 1945-10-18 1961-03-28 Clarence N Hickman Separation means
US2519878A (en) * 1946-07-31 1950-08-22 Carold F Bjork Rocket projectile
US2603061A (en) * 1946-08-20 1952-07-15 William H Avery Rocket loading arrangement
US3033117A (en) * 1948-06-17 1962-05-08 Hercules Powder Co Ltd Propellent charge
US2694364A (en) * 1949-01-18 1954-11-16 Lyle K Liljegren Streamlined mortar shell
US2853946A (en) * 1954-01-26 1958-09-30 Unexcelled Chemical Corp Rockets
US2939275A (en) * 1954-02-24 1960-06-07 Unexcelled Chemical Corp Solid-fuel rocket type motor assemblies
BE545501A (en) * 1955-03-02
US2946261A (en) * 1956-05-02 1960-07-26 Sydney R Crockett Peripheral nozzle spinner rocket
US3077734A (en) * 1956-12-10 1963-02-19 Phillips Petroleum Co Solid-propellant rocket motor
BE554364A (en) * 1957-01-15
DE977712C (en) * 1957-03-03 1968-08-08 Franz Rudolf Dipl-Ing Thomanek A missile-powered missile equipped with a lined shaped charge
DE1097321B (en) * 1957-04-10 1961-01-12 Financ D Expansion Commerciale Supersonic velocity projectile
US3105350A (en) * 1959-02-26 1963-10-01 Thompson Ramo Wooldridge Inc Monofuel propellant booster rocket
FR2479905A1 (en) * 1980-04-03 1981-10-09 France Etat Rocket solid propellant charge - is partially housed in case with ignition and priming
GB8324900D0 (en) * 1983-09-16 1983-10-19 Secr Defence Rocket motors
US7096791B2 (en) * 2002-07-12 2006-08-29 Arthur Vanmoor Projectile with improved dynamic shape

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503271A (en) * 1945-02-06 1950-04-11 Clarence N Hickman Rocket projectile
US2613605A (en) * 1946-11-09 1952-10-14 Energa Projectile
US2479718A (en) * 1947-01-29 1949-08-23 Carold F Bjork Rocket projectile
US2690314A (en) * 1949-12-15 1954-09-28 Us Navy Long-range guided athodyd
US2701525A (en) * 1952-04-03 1955-02-08 Clarence N Hickman Mortar shell loading driver rocket
US3144828A (en) * 1962-06-30 1964-08-18 Rheinmetall Gmbh Spin-stabilized rocket projectile
US3277825A (en) * 1963-11-07 1966-10-11 Brevets Aero Mecaniques Self-propelled armor-piercing shells
US3807275A (en) * 1972-10-06 1974-04-30 Us Army Miniature missile system
FR2412812A1 (en) * 1977-12-23 1979-07-20 Rheinmetall Gmbh DEVICE ALLOWING TO MODIFY THE TRAJECTORY OF A PROJECTILE

Also Published As

Publication number Publication date
GB516463A (en) 1940-01-02
CH208567A (en) 1940-02-15
GB516865A (en) 1940-01-12
BE428854A (en)
FR839861A (en) 1939-04-13

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