GB982440A - Rocket propelled missile - Google Patents
Rocket propelled missileInfo
- 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
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.
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)
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)
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)
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 |
-
1956
- 1956-07-30 US US600859A patent/US3167016A/en not_active Expired - Lifetime
-
1957
- 1957-07-30 GB GB24209/57A patent/GB982440A/en not_active Expired
Cited By (2)
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 |
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