GB868326A - Rocket motor propelled bomb - Google Patents
Rocket motor propelled bombInfo
- Publication number
- GB868326A GB868326A GB7764/60A GB776460A GB868326A GB 868326 A GB868326 A GB 868326A GB 7764/60 A GB7764/60 A GB 7764/60A GB 776460 A GB776460 A GB 776460A GB 868326 A GB868326 A GB 868326A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bomb
- valves
- fired
- rocket motor
- 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
Links
- 230000009172 bursting Effects 0.000 abstract 1
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
- F42B15/22—Missiles having a trajectory finishing below water surface
-
- 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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/92—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust
-
- 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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
-
- 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
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/12—Propulsion specially adapted for torpedoes
- F42B19/26—Propulsion specially adapted for torpedoes by jet propulsion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B21/00—Depth charges
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Testing Of Engines (AREA)
- Radar Systems Or Details Thereof (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
868,326. Self-propelled missiles. BOFORS A. B. March 4, 1960 [March 21, 1959], No. 7764/60. Class 9(2). A rocket motor propelled bomb 1 is adapted to be fired with one of at least two velocities, and the front part of the motor is provided with controlled exhaust channels 15,16, which emerge at the front end of the bomb through nozzles 19, 20 respectively. Rocket charges 5, 6 in a chamber 10 are divided by a wall 9. Charge 5 may be fired alone with four exhaust valves 12 open, the retaining piston 13 having been moved to the open position by a bursting charge 14, or with the valves 12 closed, or both charges 5, 6 may be fired together with the valves closed, each method giving progressively higher launching velocity.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE273659 | 1959-03-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB868326A true GB868326A (en) | 1961-05-17 |
Family
ID=20367034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7764/60A Expired GB868326A (en) | 1959-03-21 | 1960-03-04 | Rocket motor propelled bomb |
Country Status (6)
Country | Link |
---|---|
US (1) | US2989919A (en) |
BE (1) | BE588749A (en) |
DE (1) | DE1130734B (en) |
FR (1) | FR1251728A (en) |
GB (1) | GB868326A (en) |
NL (2) | NL110668C (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3251267A (en) * | 1963-06-18 | 1966-05-17 | Emerson Electric Co | Spin rocket and launcher |
US9823053B1 (en) * | 2016-08-29 | 2017-11-21 | The Boeing Company | Solid-fuel ramjet ammunition |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR498378A (en) * | 1915-05-10 | 1920-01-09 | Max De Watteville | Projectile |
FR525867A (en) * | 1917-06-04 | 1921-09-28 | Louis Ferdinand Bourguignon | Message shells |
DE568066C (en) * | 1930-08-02 | 1933-01-13 | Elek Sche App M B H Ges | Control for missiles and similar projectiles |
US2941470A (en) * | 1955-03-02 | 1960-06-21 | Brandt Soc Nouv Ets | Self-propelled projectile |
US2850976A (en) * | 1955-06-28 | 1958-09-09 | Howard S Seifert | Thrust cancellation device for use in solid propellant rocket |
US2856851A (en) * | 1955-07-27 | 1958-10-21 | Harold E Thomas | Apparatus for zoning rockets |
-
0
- NL NL249367D patent/NL249367A/xx unknown
-
1960
- 1960-03-03 DE DEA34124A patent/DE1130734B/en active Pending
- 1960-03-04 GB GB7764/60A patent/GB868326A/en not_active Expired
- 1960-03-12 NL NL249367A patent/NL110668C/xx active
- 1960-03-17 BE BE588749A patent/BE588749A/en unknown
- 1960-03-18 FR FR821830A patent/FR1251728A/en not_active Expired
- 1960-03-21 US US16370A patent/US2989919A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
NL249367A (en) | |
BE588749A (en) | 1960-07-18 |
US2989919A (en) | 1961-06-27 |
DE1130734B (en) | 1962-05-30 |
NL110668C (en) | 1964-09-15 |
FR1251728A (en) | 1961-01-20 |
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