ES336633A1 - Rifle grenade - Google Patents
Rifle grenadeInfo
- Publication number
- ES336633A1 ES336633A1 ES336633A ES336633A ES336633A1 ES 336633 A1 ES336633 A1 ES 336633A1 ES 336633 A ES336633 A ES 336633A ES 336633 A ES336633 A ES 336633A ES 336633 A1 ES336633 A1 ES 336633A1
- Authority
- ES
- Spain
- Prior art keywords
- tail tube
- grenade
- rifle
- warhead
- piston
- 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
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
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- 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
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/04—Rifle grenades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/10—Cartridges, i.e. cases with charge and missile with self-propelled bullet
- F42B5/105—Cartridges, i.e. cases with charge and missile with self-propelled bullet propelled by two propulsive charges, the rearwardly situated one being separated from the rest of the projectile during flight or in the barrel; Projectiles with self-ejecting cartridge cases
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Telescopes (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Rifle grenade comprising a warhead 2 containing a propellant charge 25, and a tail tube 3 releasably coupled to the warhead through a fracturable shank 6 of a piston 5 formed with a striker 4 for igniting a detonating cartridge 21. On launching the grenade, the gas pressure produced on ignition of a firing charge in a rifle drives the piston forwards to fracture the shank and release the tail tube, the continued displacement of the piston causing the striker to ignite the detonating cartridge and thereby the propellant charge. Part of the gases from the rifle pass through tangential nozzles formed in an end plate 15 of the tail tube and impart spin to the grenade. The combustion gases from the propellant charge impinge upon the plate 15 and facilitate separation of the warhead and the tail tube.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEJ0030404 | 1966-03-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES336633A1 true ES336633A1 (en) | 1968-01-01 |
Family
ID=7203875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES336633A Expired ES336633A1 (en) | 1966-03-22 | 1967-02-09 | Rifle grenade |
Country Status (8)
Country | Link |
---|---|
US (1) | US3388666A (en) |
BE (1) | BE695268A (en) |
CH (1) | CH472018A (en) |
ES (1) | ES336633A1 (en) |
FR (1) | FR1508558A (en) |
GB (1) | GB1165802A (en) |
NL (2) | NL6700671A (en) |
SE (1) | SE333527B (en) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH520316A (en) * | 1970-02-27 | 1972-03-15 | Oerlikon Buehrle Ag | Spin-stabilized missile projectile |
US3750581A (en) * | 1971-09-20 | 1973-08-07 | Us Army | Missile motor igniter assembly |
US3981225A (en) * | 1973-05-29 | 1976-09-21 | Smith Matthew S | Launcher arrangement for rocket powered round |
US3880044A (en) * | 1973-07-05 | 1975-04-29 | Us Army | Muzzle attachment for accelerating a projectle |
US3960084A (en) * | 1973-08-08 | 1976-06-01 | Fabrique Nationale Herstal S.A. En Abrege Fn | Fuse for rifle-grenade |
US3949676A (en) * | 1974-06-10 | 1976-04-13 | The United States Of America As Represented By The Secretary Of The Navy | Load actuated electro-ignition circuit switch |
US3952664A (en) * | 1974-06-10 | 1976-04-27 | The United States Of America As Represented By The Secretary Of The Navy | Rocket nozzle multi function |
US4023499A (en) * | 1975-01-07 | 1977-05-17 | Fabrique Nationale Herstal S.A. | Fuse for rifle-grenade |
US4099465A (en) * | 1976-12-17 | 1978-07-11 | The United States Of America As Represented By The Secretary Of The Navy | Ignition device for missile motors |
FR2398998A1 (en) * | 1977-07-26 | 1979-02-23 | Serat | Firearm-launched self-propelled missile - has additional propellant charge with nozzle axes converging on its own |
FR2448706A1 (en) * | 1979-02-09 | 1980-09-05 | Luchaire Sa | Hand-weapon fired anti-tank missile - with extra propellant fired after launching to rotate missile and improve range and stability |
GR68779B (en) * | 1981-11-16 | 1982-02-18 | Karampateas Eustratios | |
DE3510446A1 (en) * | 1985-03-22 | 1986-09-25 | Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co KG, 2077 Trittau | DRIVE SET FOR SOIL REDUCTION |
US5431106A (en) * | 1985-06-05 | 1995-07-11 | Shorts Missile Systems Limited | Release of daughter missiles |
US4886223A (en) * | 1988-05-31 | 1989-12-12 | Honeywell Inc. | Projectile with spin chambers |
DE4210113C1 (en) * | 1992-03-27 | 1998-11-05 | Athanassios Dr Ing Zacharias | Method of steering flying body for elongated munitions launched from overhead, e.g. from helicopter |
SE501082C2 (en) * | 1993-03-30 | 1994-11-07 | Bofors Ab | Method and apparatus for giving an airborne combat section a desired pattern of movement |
WO2016032354A1 (en) * | 2014-08-26 | 2016-03-03 | Ренат Абдульберович ЮСУПОВ | Caliber shell with rigid mounting to housing of stabilizing fins |
US9664142B1 (en) * | 2016-05-11 | 2017-05-30 | Jian-Lin Huang | Rocket structure |
US11306997B2 (en) * | 2020-08-11 | 2022-04-19 | Jian-Lin Huang | Throwing device with two-stage propulsion system |
US11346640B2 (en) * | 2020-08-11 | 2022-05-31 | Jian-Lin Huang | Two-stage propulsion system |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR714636A (en) * | 1930-07-25 | 1931-11-25 | Pomegranate enhancements | |
US2415803A (en) * | 1944-12-23 | 1947-02-18 | Abell Royal Allen | Cartridge |
NL108359C (en) * | 1958-03-28 | Energa | ||
NL251775A (en) * | 1959-05-21 | |||
NL122936C (en) * | 1960-05-05 | |||
US3140660A (en) * | 1961-12-07 | 1964-07-14 | Brevets Aero Mecaniques | Grenades comprising a booster and similar devices to be launched by a firearm |
US3204559A (en) * | 1962-12-31 | 1965-09-07 | Avco Corp | Rocket propellant charge igniter |
-
0
- NL NL135093D patent/NL135093C/xx active
-
1967
- 1967-01-16 NL NL6700671A patent/NL6700671A/xx unknown
- 1967-01-18 GB GB2583/67A patent/GB1165802A/en not_active Expired
- 1967-01-18 FR FR91593A patent/FR1508558A/en not_active Expired
- 1967-02-09 ES ES336633A patent/ES336633A1/en not_active Expired
- 1967-03-09 BE BE695268D patent/BE695268A/xx unknown
- 1967-03-13 CH CH358667A patent/CH472018A/en not_active IP Right Cessation
- 1967-03-15 US US623303A patent/US3388666A/en not_active Expired - Lifetime
- 1967-03-21 SE SE03933/67A patent/SE333527B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
FR1508558A (en) | 1968-01-05 |
BE695268A (en) | 1967-09-11 |
CH472018A (en) | 1969-04-30 |
US3388666A (en) | 1968-06-18 |
NL6700671A (en) | 1967-09-25 |
NL135093C (en) | |
GB1165802A (en) | 1969-10-01 |
SE333527B (en) | 1971-03-15 |
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