IL79864A - Detachable mechanism for creating a directed thrust for an aeronautical vehicle - Google Patents
Detachable mechanism for creating a directed thrust for an aeronautical vehicleInfo
- Publication number
- IL79864A IL79864A IL7986486A IL7986486A IL79864A IL 79864 A IL79864 A IL 79864A IL 7986486 A IL7986486 A IL 7986486A IL 7986486 A IL7986486 A IL 7986486A IL 79864 A IL79864 A IL 79864A
- Authority
- IL
- Israel
- Prior art keywords
- missile
- detachable
- propulsion means
- thrust
- auxiliary
- Prior art date
Links
- 230000007246 mechanism Effects 0.000 title claims description 18
- 230000004044 response Effects 0.000 claims description 5
- 230000033001 locomotion Effects 0.000 claims description 3
- 230000002457 bidirectional effect Effects 0.000 claims 2
- 238000010304 firing Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 230000009471 action Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000026058 directional locomotion Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 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
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
-
- 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
- F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile
-
- 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
- F42B15/10—Missiles having a trajectory only in the air
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Mechanical Control Devices (AREA)
- Details Of Aerials (AREA)
- Transmission Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US80144585A | 1985-11-25 | 1985-11-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
IL79864A0 IL79864A0 (en) | 1986-11-30 |
IL79864A true IL79864A (en) | 1994-05-30 |
Family
ID=25181115
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL7986486A IL79864A (en) | 1985-11-25 | 1986-08-27 | Detachable mechanism for creating a directed thrust for an aeronautical vehicle |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0227211B1 (de) |
JP (1) | JP2593454B2 (de) |
KR (1) | KR930002105B1 (de) |
DE (1) | DE3678542D1 (de) |
IL (1) | IL79864A (de) |
NO (1) | NO162583C (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2272047B (en) * | 1989-12-14 | 1994-07-27 | British Aerospace | Stand-off weapons |
IL115749A (en) * | 1994-10-27 | 2000-02-29 | Thomson Csf | Missile launching and orientating system |
DE19828645C1 (de) * | 1998-06-26 | 1999-11-18 | Buck Werke Gmbh & Co I K | Flugkörper zur Bekämpfung feststehender und/oder beweglicher Ziele |
KR101159648B1 (ko) * | 2011-07-29 | 2012-06-25 | 삼성탈레스 주식회사 | 제트엔진이 탑재된 미사일 기만기 |
FR2997179B1 (fr) * | 2012-10-22 | 2015-01-16 | Roxel France | Dispositif combine de pilotage de trajectoire et de reduction de trainee. |
GB2616727B (en) * | 2022-02-10 | 2024-05-08 | Mbda Uk Ltd | Apparatus for providing an interface between a missile and a launch platform |
IL301400A (en) * | 2023-03-15 | 2024-10-01 | Israel Aerospace Ind Ltd | A module for a missile |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1125143A (fr) * | 1955-04-27 | 1956-10-24 | Artifices Titan Soc D | Fusée à propulseur larguable |
US3224370A (en) * | 1959-07-27 | 1965-12-21 | Curtiss Wright Corp | Booster rocket |
US3067682A (en) * | 1960-02-18 | 1962-12-11 | Aerojet General Co | Gyro pull rocket |
GB1269272A (en) * | 1968-06-06 | 1972-04-06 | Messeschmitt Bolkow Blohm Gmbh | Improvements in multi-stage rockets |
US4044970A (en) * | 1975-08-08 | 1977-08-30 | General Dynamics Corporation | Integrated thrust vector aerodynamic control surface |
DE2721656A1 (de) | 1977-05-13 | 1978-11-16 | Ver Flugtechnische Werke | Stellanordnung zur steuerung von flugkoerpern |
US4364530A (en) * | 1980-09-08 | 1982-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Propulsion/control modular booster |
DE3133339A1 (de) * | 1981-08-22 | 1983-03-10 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | "unbemannter, aus einem transportbehaelter zu startender flugkoerper" |
-
1986
- 1986-08-27 IL IL7986486A patent/IL79864A/en not_active IP Right Cessation
- 1986-08-28 NO NO863455A patent/NO162583C/no not_active IP Right Cessation
- 1986-09-02 DE DE8686306764T patent/DE3678542D1/de not_active Expired - Fee Related
- 1986-09-02 EP EP86306764A patent/EP0227211B1/de not_active Expired - Lifetime
- 1986-09-12 JP JP61215606A patent/JP2593454B2/ja not_active Expired - Lifetime
- 1986-09-20 KR KR1019860007884A patent/KR930002105B1/ko not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP0227211B1 (de) | 1991-04-03 |
NO162583B (no) | 1989-10-09 |
KR930002105B1 (ko) | 1993-03-26 |
NO162583C (no) | 1990-01-17 |
IL79864A0 (en) | 1986-11-30 |
KR870005231A (ko) | 1987-06-05 |
NO863455D0 (no) | 1986-08-28 |
EP0227211A1 (de) | 1987-07-01 |
JPS62125300A (ja) | 1987-06-06 |
JP2593454B2 (ja) | 1997-03-26 |
DE3678542D1 (de) | 1991-05-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
KB | Patent renewed | ||
HC | Change of name of proprietor(s) | ||
KB | Patent renewed | ||
MM9K | Patent not in force due to non-payment of renewal fees |