SE421959B - Raket med avskiljbara steg - Google Patents
Raket med avskiljbara stegInfo
- Publication number
- SE421959B SE421959B SE7714510A SE7714510A SE421959B SE 421959 B SE421959 B SE 421959B SE 7714510 A SE7714510 A SE 7714510A SE 7714510 A SE7714510 A SE 7714510A SE 421959 B SE421959 B SE 421959B
- Authority
- SE
- Sweden
- Prior art keywords
- charge
- front wall
- rocket
- rocket according
- sliding part
- Prior art date
Links
Classifications
-
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7639280A FR2376301A1 (fr) | 1976-12-28 | 1976-12-28 | Engin autopropulse a etages separables |
Publications (2)
Publication Number | Publication Date |
---|---|
SE7714510L SE7714510L (sv) | 1978-06-29 |
SE421959B true SE421959B (sv) | 1982-02-08 |
Family
ID=9181619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7714510A SE421959B (sv) | 1976-12-28 | 1977-12-20 | Raket med avskiljbara steg |
Country Status (5)
Country | Link |
---|---|
US (1) | US4198896A (xx) |
DE (1) | DE2757807C2 (xx) |
FR (1) | FR2376301A1 (xx) |
GB (1) | GB1543689A (xx) |
SE (1) | SE421959B (xx) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS56159535A (en) * | 1980-05-13 | 1981-12-08 | Nissan Motor Co Ltd | Rocket motor |
DE3133339A1 (de) * | 1981-08-22 | 1983-03-10 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | "unbemannter, aus einem transportbehaelter zu startender flugkoerper" |
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 |
DE3686321T2 (de) * | 1985-10-31 | 1992-12-17 | British Aerospace | Ausstossantrieb fuer flugkoerper. |
US5001982A (en) * | 1988-06-28 | 1991-03-26 | General Dynamics Corp., Pomona Division | Anti-armor weapon |
FR2650639B1 (fr) * | 1989-08-04 | 1991-09-27 | Thomson Brandt Armements | Systeme de fixation deverrouillable pour deux elements notamment de munition |
IL115749A (en) * | 1994-10-27 | 2000-02-29 | Thomson Csf | Missile launching and orientating system |
GB2402462B (en) * | 2000-10-31 | 2005-08-31 | Saab Ab | Method and device for a multiple step rocket |
US7958825B2 (en) * | 2007-09-24 | 2011-06-14 | Raytheon Company | System and method for integrated stage separation |
US8534174B2 (en) * | 2010-09-27 | 2013-09-17 | Power Tool Institute | Pyrotechnic actuator and power cutting tool with safety reaction system having such pyrotechnic actuator |
US10577129B1 (en) * | 2015-05-19 | 2020-03-03 | Peter Davis Poulsen | Apparatus and methods for launching a payload |
IL260886B (en) * | 2018-07-30 | 2021-04-29 | Rafael Advanced Defense Systems Ltd | Rocket armament that can be launched from a tubular launcher with non-ignition security outside the launcher and engine separation in flight |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1328459A (fr) * | 1962-04-18 | 1963-05-31 | Soc Tech De Rech Ind | Roquette à propulseur largable |
FR1435514A (fr) * | 1964-06-05 | 1966-04-15 | British Aircraft Corp Ltd | Dispositif de séparation entre un satellite et sa fusée porteuse |
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 |
US3491692A (en) * | 1967-02-18 | 1970-01-27 | Bolkow Gmbh | Multi-stage rocket |
US4023496A (en) * | 1972-08-09 | 1977-05-17 | The United States Of America As Represented By The Secretary Of The Army | Ejector motor braking system |
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 |
US4050351A (en) * | 1976-05-04 | 1977-09-27 | Societe Anonyme Dite: Societe Europeenne Depropulsion | Assembly for launching a projectile |
-
1976
- 1976-12-28 FR FR7639280A patent/FR2376301A1/fr active Granted
-
1977
- 1977-12-20 SE SE7714510A patent/SE421959B/sv not_active IP Right Cessation
- 1977-12-23 DE DE2757807A patent/DE2757807C2/de not_active Expired
- 1977-12-23 GB GB54009/77A patent/GB1543689A/en not_active Expired
- 1977-12-28 US US05/865,025 patent/US4198896A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2376301B1 (xx) | 1979-07-13 |
DE2757807A1 (de) | 1978-08-24 |
GB1543689A (en) | 1979-04-04 |
FR2376301A1 (fr) | 1978-07-28 |
DE2757807C2 (de) | 1986-07-24 |
US4198896A (en) | 1980-04-22 |
SE7714510L (sv) | 1978-06-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SE421959B (sv) | Raket med avskiljbara steg | |
US2684629A (en) | Reaction-motor missile | |
US2850976A (en) | Thrust cancellation device for use in solid propellant rocket | |
US4335657A (en) | Ammunition round with retained piston | |
US3237402A (en) | Variable thrust nozzle | |
SE438377B (sv) | Teleskopartad hylslos ammunition | |
US2814929A (en) | Fuel supply control for rocket type jet propulsion units | |
RU2486452C1 (ru) | Способ увеличения дальности полета артиллерийского снаряда и устройство для его реализации | |
US3070018A (en) | Nose cone ejection system | |
US3377952A (en) | Probe ejecting rocket motor | |
US3026772A (en) | Cargo launcher | |
US3115008A (en) | Integral rocket ramjet missile propulsion system | |
US3063240A (en) | Booster means for a ramjetrocket device | |
GB1605304A (en) | Rockets | |
US3132475A (en) | Hybrid rocket propulsion system | |
US4154141A (en) | Ultrafast, linearly-deflagration ignition system | |
US3023704A (en) | Projectiles for mortars and like projectors | |
US3329089A (en) | Retention-release mechanism for reaction motors and rocket interstages | |
US2752850A (en) | Self-propelled missile | |
US4250705A (en) | Apparatus for the connection between two stages of a self-propelled engine | |
US3357187A (en) | Ducted rocket motor | |
US4327885A (en) | Thrust augmented rocket | |
US3438303A (en) | System including a tubular launching tube and a rocket provided with an outer auxiliary launching charge | |
US3951342A (en) | Extendible nozzle for a rocket motor or the like | |
US3035796A (en) | Dual thrust rocket booster tube |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAL | Patent in force |
Ref document number: 7714510-0 Format of ref document f/p: F |
|
NUG | Patent has lapsed |
Ref document number: 7714510-0 Format of ref document f/p: F |