DE1220288C2 - - Google Patents
Info
- Publication number
- DE1220288C2 DE1220288C2 DE1963T0024455 DET0024455A DE1220288C2 DE 1220288 C2 DE1220288 C2 DE 1220288C2 DE 1963T0024455 DE1963T0024455 DE 1963T0024455 DE T0024455 A DET0024455 A DE T0024455A DE 1220288 C2 DE1220288 C2 DE 1220288C2
- Authority
- DE
- Germany
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
- F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
-
- 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
-
- 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
- F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
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)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Testing Of Engines (AREA)
- Special Conveying (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US216203A US3246468A (en) | 1962-08-10 | 1962-08-10 | Steering means for rockets |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE1220288B DE1220288B (de) | 1966-06-30 |
| DE1220288C2 true DE1220288C2 (en:Method) | 1967-01-19 |
Family
ID=22806152
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DET24455A Granted DE1220288B (de) | 1962-08-10 | 1963-08-08 | Ablenkvorrichtung fuer Raketenduesenstrahlen |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3246468A (en:Method) |
| DE (1) | DE1220288B (en:Method) |
| FR (1) | FR1365790A (en:Method) |
| GB (1) | GB1045885A (en:Method) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE396135B (sv) * | 1972-07-31 | 1977-09-05 | Bofors Ab | Styranordning for raketmotordrivna projektiler |
| NZ198917A (en) * | 1980-11-14 | 1985-01-31 | Commw Of Australia | Rocket controlled by spoiler tabs in exhaust |
| US5072891A (en) * | 1989-11-22 | 1991-12-17 | Applied Technology Associates | Combination actuator and coolant supply for missile and rocket vector control |
| DE102008022289B4 (de) * | 2008-04-25 | 2010-07-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1879187A (en) * | 1931-02-07 | 1932-09-27 | Robert H Goddard | Mechanism for directing flight |
| CH316187A (fr) * | 1951-08-02 | 1956-09-30 | Zborowski Helmut Ph G A R Von | Aérodyne |
| US2945344A (en) * | 1956-10-23 | 1960-07-19 | Phillips Petroleum Co | Gas generator adapted for on-off operation |
| US3026806A (en) * | 1957-03-22 | 1962-03-27 | Russell Mfg Co | Ballistic missile nose cone |
| US3036430A (en) * | 1958-06-19 | 1962-05-29 | Snecma | Jet control apparatus |
| US3096049A (en) * | 1960-01-25 | 1963-07-02 | Edward S Karasinski | Steering means for space vehicles missiles and high altitude flying craft |
| US3022190A (en) * | 1960-02-15 | 1962-02-20 | Emerson Electric Mfg Co | Process of and composition for controlling temperatures |
-
1962
- 1962-08-10 US US216203A patent/US3246468A/en not_active Expired - Lifetime
-
1963
- 1963-07-25 GB GB29526/63A patent/GB1045885A/en not_active Expired
- 1963-08-08 DE DET24455A patent/DE1220288B/de active Granted
- 1963-08-08 FR FR944162A patent/FR1365790A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US3246468A (en) | 1966-04-19 |
| DE1220288B (de) | 1966-06-30 |
| FR1365790A (fr) | 1964-07-03 |
| GB1045885A (en) | 1966-10-19 |