SE7714509L - Forbindelseanordning mellan stegen i en sjelvdriven missil - Google Patents
Forbindelseanordning mellan stegen i en sjelvdriven missilInfo
- Publication number
- SE7714509L SE7714509L SE7714509A SE7714509A SE7714509L SE 7714509 L SE7714509 L SE 7714509L SE 7714509 A SE7714509 A SE 7714509A SE 7714509 A SE7714509 A SE 7714509A SE 7714509 L SE7714509 L SE 7714509L
- Authority
- SE
- Sweden
- Prior art keywords
- stage
- stages
- self
- pyrotechnic charge
- front stage
- 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
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- 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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/20—Shape or structure of solid propellant charges of the external-burning type
-
- 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
- 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
- F02K9/97—Rocket nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air Bags (AREA)
- Platform Screen Doors And Railroad Systems (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7639278A FR2376300A1 (fr) | 1976-12-28 | 1976-12-28 | Dispositif pour la liaison entre deux etages d'un engin autopropulse |
Publications (2)
Publication Number | Publication Date |
---|---|
SE7714509L true SE7714509L (sv) | 1978-06-29 |
SE421831B SE421831B (sv) | 1982-02-01 |
Family
ID=9181617
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7714509A SE421831B (sv) | 1976-12-28 | 1977-12-20 | Forbindningsanordning mellan raketsteg |
Country Status (7)
Country | Link |
---|---|
US (1) | US4250705A (sv) |
BE (1) | BE862427A (sv) |
DE (1) | DE2757806C2 (sv) |
FR (1) | FR2376300A1 (sv) |
GB (1) | GB1543690A (sv) |
IT (1) | IT1091528B (sv) |
SE (1) | SE421831B (sv) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2544020B1 (fr) * | 1983-04-05 | 1989-04-21 | British Aerospace | Moyen permettant la separation en vol des etages des moteurs d'un projectile |
FR2584456B1 (fr) * | 1985-07-03 | 1987-10-02 | Poudres & Explosifs Ste Nale | Dispositif de fermeture temporaire d'un orifice interne d'un propulseur |
EP0229457B1 (en) * | 1985-10-31 | 1991-03-13 | British Aerospace Public Limited Company | Missile flare |
US4803928A (en) * | 1986-08-02 | 1989-02-14 | Stefan Kramer | Tandem charge projectile |
DE3718716C2 (de) * | 1986-08-02 | 1988-06-30 | Messerschmitt Boelkow Blohm | Geschoss |
FR2613824B1 (fr) * | 1987-04-10 | 1993-05-28 | Lacroix E Tous Artifices | Roquette autopropulsee et dispositif pyrotechnique de lancement incorporant celle-ci |
DE69129815T2 (de) * | 1990-01-16 | 1998-12-03 | Tda Armements Sas | Penetratormunition für Ziele mit hohem mechanischem Widerstand |
FR2657158B1 (fr) * | 1990-01-16 | 1994-05-27 | Thomson Brandt Armements | Munition perforante pour cible a haute resistance mecanique. |
IL115749A (en) * | 1994-10-27 | 2000-02-29 | Thomson Csf | Missile launching and orientating system |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH196392A (fr) * | 1936-12-31 | 1938-03-15 | Sageb Societe Anonyme De Gesti | Projectile muni d'une fusée percutante. |
US2458475A (en) * | 1943-04-02 | 1949-01-04 | Charles C Lauritsen | Rocket device |
US2421522A (en) * | 1944-08-23 | 1947-06-03 | Winslow B Pope | Rocket projector and projectile |
US2724237A (en) * | 1946-03-05 | 1955-11-22 | Clarence N Hickman | Rocket projectile having discrete flight initiating and sustaining chambers |
FR1291041A (fr) * | 1961-03-10 | 1962-04-20 | Hotchkiss Brandt | Dispositif éjectable d'obturation et d'allumage pour projectile autopropulsé et projectile en comportant application |
FR1328459A (fr) * | 1962-04-18 | 1963-05-31 | Soc Tech De Rech Ind | Roquette à propulseur largable |
US3136872A (en) * | 1962-07-23 | 1964-06-09 | Lloyd J Banaszak | Gas operated ignition switch for a multi-stage rocket propelled missile |
FR1435514A (fr) * | 1964-06-05 | 1966-04-15 | British Aircraft Corp Ltd | Dispositif de séparation entre un satellite et sa fusée porteuse |
FR1513277A (fr) * | 1966-07-27 | 1968-02-16 | Hotchkiss Brandt | Procédé pour l'envoi d'un engin dans l'espace et engin adapté pour la mise en oeuvre de ce procédé |
US3438303A (en) * | 1966-11-30 | 1969-04-15 | Bombrini Parodi Delfino Spa | System including a tubular launching tube and a rocket provided with an outer auxiliary launching charge |
BE757634A (fr) * | 1969-10-17 | 1971-04-01 | Bofors Ab | Dispositif d'allumage pour un projectile assiste d'une fusee |
FR2260078A1 (en) * | 1973-07-05 | 1975-08-29 | Luchaire Sa | Auxiliary charge for rocket launcher - has partition forming chamber ahead of launching member for extra acceleration |
-
1976
- 1976-12-28 FR FR7639278A patent/FR2376300A1/fr active Granted
-
1977
- 1977-12-20 SE SE7714509A patent/SE421831B/sv not_active IP Right Cessation
- 1977-12-22 IT IT69889/77A patent/IT1091528B/it active
- 1977-12-23 DE DE2757806A patent/DE2757806C2/de not_active Expired
- 1977-12-23 GB GB54010/77A patent/GB1543690A/en not_active Expired
- 1977-12-28 US US05/865,026 patent/US4250705A/en not_active Expired - Lifetime
- 1977-12-28 BE BE183931A patent/BE862427A/xx not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
BE862427A (fr) | 1978-06-28 |
IT1091528B (it) | 1985-07-06 |
SE421831B (sv) | 1982-02-01 |
DE2757806A1 (de) | 1978-07-13 |
DE2757806C2 (de) | 1986-07-10 |
US4250705A (en) | 1981-02-17 |
FR2376300B1 (sv) | 1981-11-06 |
GB1543690A (en) | 1979-04-04 |
FR2376300A1 (fr) | 1978-07-28 |
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