SE340417B - - Google Patents
Info
- Publication number
- SE340417B SE340417B SE08063/69A SE806369A SE340417B SE 340417 B SE340417 B SE 340417B SE 08063/69 A SE08063/69 A SE 08063/69A SE 806369 A SE806369 A SE 806369A SE 340417 B SE340417 B SE 340417B
- Authority
- SE
- Sweden
- Prior art keywords
- missile
- fuel
- fuel charges
- jet nozzles
- propulsion motor
- Prior art date
Links
Classifications
-
- 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
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- 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
- F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Abstract
The invention concerns a missile, in particular a guided missile, having stabilizing wings and a solid fuel propulsion motor. The fuel of the propulsion motor is divided into two separate fuel charges located axially spaced in the missile. The portion of the interior of the missile between the two fuel charges consists of an empty space, into which the fuel charges deliver their combustion gases and which is surrounded by an annular member forming the external shell of the missile between the two fuel charges and comprising the jet nozzles for the propulsion motor. The two fuel charges have such relative sizes and locations in the missile that their common gravity center coincides substantially with the total gravity center of the missile. The stabilizing wings are attached to the annular member comprising the jet nozzles and are located circumferentially between said jet nozzles.
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE08063/69A SE340417B (en) | 1969-06-06 | 1969-06-06 | |
US41373A US3684215A (en) | 1969-06-06 | 1970-05-28 | Missile |
NL7007998.A NL161255C (en) | 1969-06-06 | 1970-06-02 | PROJECTILE. |
CH832570A CH508863A (en) | 1969-06-06 | 1970-06-03 | Missile with stabilizing wings and solid-state propulsion device |
NO2161/70A NO125748B (en) | 1969-06-06 | 1970-06-03 | |
JP45048661A JPS4810360B1 (en) | 1969-06-06 | 1970-06-04 | |
DE2027371A DE2027371C3 (en) | 1969-06-06 | 1970-06-04 | Missile with stabilizing wings and a solid fuel engine with two separate propellants |
BE751547D BE751547A (en) | 1969-06-06 | 1970-06-05 | MISSILE GUIDE |
GB2737770A GB1311747A (en) | 1969-06-06 | 1970-06-05 | Missile |
FR7020862A FR2049166B1 (en) | 1969-06-06 | 1970-06-05 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE08063/69A SE340417B (en) | 1969-06-06 | 1969-06-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
SE340417B true SE340417B (en) | 1971-11-15 |
Family
ID=20273043
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE08063/69A SE340417B (en) | 1969-06-06 | 1969-06-06 |
Country Status (10)
Country | Link |
---|---|
US (1) | US3684215A (en) |
JP (1) | JPS4810360B1 (en) |
BE (1) | BE751547A (en) |
CH (1) | CH508863A (en) |
DE (1) | DE2027371C3 (en) |
FR (1) | FR2049166B1 (en) |
GB (1) | GB1311747A (en) |
NL (1) | NL161255C (en) |
NO (1) | NO125748B (en) |
SE (1) | SE340417B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2463909B1 (en) * | 1979-08-17 | 1985-10-25 | Thomson Brandt | METHOD OF PILOTING AND GUIDING A MISSILE, AND MISSILE PROVIDED WITH MEANS FOR IMPLEMENTING THIS METHOD |
FR2500149B1 (en) * | 1981-02-17 | 1985-12-06 | Poudres & Explosifs Ste Nale | PROPULSIVE LOADING BIREGIME WITH TRUMPET HAVING A STAR SECTION |
GB2172383B (en) * | 1981-06-04 | 1987-08-12 | Aerospatiale | Guided missile system |
FR2578665B1 (en) * | 1981-06-04 | 1988-02-12 | Aerospatiale | LOW SPEED MISSILE PILOTING METHOD, WEAPON AND MISSILE SYSTEM FOR IMPLEMENTING THE METHOD |
FR2863665B1 (en) * | 1988-10-12 | 2007-03-30 | Aerospatiale | STATOREACTOR HAVING A TUBULAR AND MISSILE STRUCTURE PROPULATED BY SUCH STATOREACTOR |
IL101730A (en) * | 1992-04-30 | 1995-12-31 | Israel State | Moving body such as missile having wings erectable upon acceleration |
US8350200B1 (en) * | 2009-03-26 | 2013-01-08 | Lockheed Martin Corporation | Passive aerosurface adjustment for static margin management |
CN108562195B (en) * | 2018-01-12 | 2019-05-24 | 北京航空航天大学 | A kind of modularization counter weight device and rocket being conveniently adjusted |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB594516A (en) * | 1940-09-04 | 1947-11-13 | Charles Dennistoun Burney | Improvements in or relating to projectiles operating with rocket propulsion |
US2503271A (en) * | 1945-02-06 | 1950-04-11 | Clarence N Hickman | Rocket projectile |
US2816721A (en) * | 1953-09-15 | 1957-12-17 | Taylor Richard John | Rocket powered aerial vehicle |
US3013494A (en) * | 1957-08-09 | 1961-12-19 | Chanut Pierre Louis Jean | Guided missile |
US3127838A (en) * | 1960-10-12 | 1964-04-07 | Bombrini Parodi Delfino Spa | Retractable blade tail unit for projectiles |
-
1969
- 1969-06-06 SE SE08063/69A patent/SE340417B/xx unknown
-
1970
- 1970-05-28 US US41373A patent/US3684215A/en not_active Expired - Lifetime
- 1970-06-02 NL NL7007998.A patent/NL161255C/en not_active IP Right Cessation
- 1970-06-03 CH CH832570A patent/CH508863A/en not_active IP Right Cessation
- 1970-06-03 NO NO2161/70A patent/NO125748B/no unknown
- 1970-06-04 JP JP45048661A patent/JPS4810360B1/ja active Pending
- 1970-06-04 DE DE2027371A patent/DE2027371C3/en not_active Expired
- 1970-06-05 BE BE751547D patent/BE751547A/en unknown
- 1970-06-05 FR FR7020862A patent/FR2049166B1/fr not_active Expired
- 1970-06-05 GB GB2737770A patent/GB1311747A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2049166B1 (en) | 1974-05-24 |
NL161255B (en) | 1979-08-15 |
GB1311747A (en) | 1973-03-28 |
US3684215A (en) | 1972-08-15 |
CH508863A (en) | 1971-06-15 |
NO125748B (en) | 1972-10-23 |
DE2027371B2 (en) | 1979-05-03 |
NL7007998A (en) | 1970-12-08 |
BE751547A (en) | 1970-11-16 |
JPS4810360B1 (en) | 1973-04-02 |
NL161255C (en) | 1980-01-15 |
DE2027371A1 (en) | 1970-12-10 |
DE2027371C3 (en) | 1980-01-03 |
FR2049166A1 (en) | 1971-03-26 |
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