IT8948113A0 - Apparecchio generatore di spinta, in particolare per guidare proiettili e missili - Google Patents
Apparecchio generatore di spinta, in particolare per guidare proiettili e missiliInfo
- Publication number
- IT8948113A0 IT8948113A0 IT8948113A IT4811389A IT8948113A0 IT 8948113 A0 IT8948113 A0 IT 8948113A0 IT 8948113 A IT8948113 A IT 8948113A IT 4811389 A IT4811389 A IT 4811389A IT 8948113 A0 IT8948113 A0 IT 8948113A0
- Authority
- IT
- Italy
- Prior art keywords
- missiles
- generating apparatus
- thrust generating
- guiding projectiles
- projectiles
- Prior art date
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
- F42B15/01—Arrangements thereon for guidance or control
-
- 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
- F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
-
- 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
-
- 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
- F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/212,468 US6315238B1 (en) | 1988-06-28 | 1988-06-28 | Thrusting apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
IT8948113A0 true IT8948113A0 (it) | 1989-06-22 |
Family
ID=22791153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8948113A IT8948113A0 (it) | 1988-06-28 | 1989-06-22 | Apparecchio generatore di spinta, in particolare per guidare proiettili e missili |
Country Status (4)
Country | Link |
---|---|
US (1) | US6315238B1 (it) |
JP (1) | JP2008255786A (it) |
GB (1) | GB2517655B (it) |
IT (1) | IT8948113A0 (it) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6752351B2 (en) * | 2002-11-04 | 2004-06-22 | The United States Of America As Represented By The Secretary Of The Navy | Low mass flow reaction jet |
US7975468B1 (en) * | 2006-09-07 | 2011-07-12 | Omnitek Partners Llc | Actuators for gun-fired projectiles and mortars |
KR100742596B1 (ko) * | 2006-02-21 | 2007-08-02 | 국방과학연구소 | 측 추력기 모듈 |
EP2085489A1 (en) * | 2008-02-02 | 2009-08-05 | Novaltec Sàrl | Fluid microjet system |
US11543835B2 (en) * | 2010-01-15 | 2023-01-03 | Lockheed Martin Corporation | Monolithic attitude control motor frame and system |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB930961A (en) * | 1961-04-11 | 1963-07-10 | Mcdonnell Aircraft Corp | Guidance system |
US3226928A (en) * | 1962-01-24 | 1966-01-04 | Hexcel Products Inc | Honeycomb rocket propellant grain |
FR2469345A1 (fr) * | 1979-11-09 | 1981-05-22 | Thomson Brandt | Procede de pilotage et de guidage de projectiles en phase terminale et projectiles comportant les moyens de mise en oeuvre de ce procede |
US4413795A (en) * | 1980-09-05 | 1983-11-08 | The Garrett Corporation | Fluidic thruster control and method |
DE3427227A1 (de) * | 1984-07-24 | 1986-01-30 | Diehl GmbH & Co, 8500 Nürnberg | Endphasen-steuerbarer munitionsartikel und verfahren zu seiner zielnavigation |
DE3521204A1 (de) * | 1985-06-13 | 1986-12-18 | Diehl GmbH & Co, 8500 Nürnberg | Impulstriebwerk |
-
1988
- 1988-06-28 US US07/212,468 patent/US6315238B1/en not_active Expired - Lifetime
-
1989
- 1989-06-22 IT IT8948113A patent/IT8948113A0/it unknown
- 1989-06-27 GB GB8914705.2A patent/GB2517655B/en not_active Expired - Lifetime
- 1989-06-28 JP JP80002089A patent/JP2008255786A/ja not_active Ceased
Also Published As
Publication number | Publication date |
---|---|
JP2008255786A (ja) | 2008-10-23 |
US6315238B1 (en) | 2001-11-13 |
GB8914705D0 (en) | 2013-11-13 |
GB2517655A (en) | 2015-03-04 |
GB2517655B (en) | 2016-03-30 |
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