BE695600A - - Google Patents
Info
- Publication number
- BE695600A BE695600A BE695600DA BE695600A BE 695600 A BE695600 A BE 695600A BE 695600D A BE695600D A BE 695600DA BE 695600 A BE695600 A BE 695600A
- Authority
- BE
- Belgium
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
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- 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
- F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases
-
- 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
- F42B10/26—Stabilising arrangements using spin
- F42B10/28—Stabilising arrangements using spin induced by gas action
- F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR54510A FR1488272A (fr) | 1966-03-22 | 1966-03-22 | Système de pilotage de missiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE695600A true BE695600A (en:Method) | 1967-09-18 |
Family
ID=8604395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE695600D BE695600A (en:Method) | 1966-03-22 | 1967-03-16 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3502288A (en:Method) |
| BE (1) | BE695600A (en:Method) |
| DE (1) | DE1578081B2 (en:Method) |
| FR (1) | FR1488272A (en:Method) |
| GB (1) | GB1185193A (en:Method) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3711013A (en) * | 1971-04-26 | 1973-01-16 | Rohr Corp | Thrust control and sound apparatus |
| US3739984A (en) * | 1971-08-25 | 1973-06-19 | Rohr Industries Inc | Thrust augmenting and south suppressing apparatus and method |
| DE2846372C2 (de) * | 1978-10-25 | 1985-11-21 | Rheinmetall GmbH, 4000 Düsseldorf | Geschoß mit radialgerichteten Steuerdüsen zur Endphasenlenkung |
| US4384690A (en) * | 1981-03-06 | 1983-05-24 | The United States Of America As Represented By The Secretary Of The Navy | Thrust vector control for large deflection angles |
| EP0245565B1 (fr) * | 1986-05-12 | 1991-03-13 | AEROSPATIALE Société Nationale Industrielle | Procédé de pilotage d'un missile à faible vitesse, système d'arme et missile pour la mise en oeuvre du procédé |
| FR2578665B1 (fr) * | 1981-06-04 | 1988-02-12 | Aerospatiale | Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede |
| FR2536720A1 (fr) * | 1982-11-29 | 1984-06-01 | Aerospatiale | Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme |
| JPH0830640B2 (ja) * | 1986-05-22 | 1996-03-27 | アエロスパテイアル・ソシエテ・ナシヨナル・アンダストリエル | ミサイル |
| US5273237A (en) * | 1992-11-02 | 1993-12-28 | The United States Of America As Represented By The Secretary Of The Air Force | Forebody nozzle for aircraft directional control |
| US8186145B2 (en) * | 2008-02-26 | 2012-05-29 | Aerojet-General Corporation | Rocket nozzles for unconventional vehicles |
| US9018572B2 (en) * | 2012-11-06 | 2015-04-28 | Raytheon Company | Rocket propelled payload with divert control system within nose cone |
| RU2558502C1 (ru) * | 2014-05-13 | 2015-08-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Поволжский государственный технологический университет" | Способ управления ракетой |
| WO2022023790A1 (en) * | 2020-07-28 | 2022-02-03 | Eijadi Ramin | Conceptual design of a modern multi-purpose actuator with the capability of performance similar to control surfaces |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2694898A (en) * | 1948-08-09 | 1954-11-23 | France Etat | Device for deflecting a high-speed jet of gas ejected through a nozzle |
| US2726510A (en) * | 1952-03-26 | 1955-12-13 | Daniel And Florence Guggenhcim | Flight-control apparatus involving steering combustion chambers |
| US3016066A (en) * | 1960-01-22 | 1962-01-09 | Raymond W Warren | Fluid oscillator |
| US3158166A (en) * | 1962-08-07 | 1964-11-24 | Raymond W Warren | Negative feedback oscillator |
| US3246863A (en) * | 1962-10-25 | 1966-04-19 | Honeywell Inc | Control apparatus |
| US3279185A (en) * | 1963-07-18 | 1966-10-18 | George D Lewis | Rocket steering system |
| US3228410A (en) * | 1963-09-30 | 1966-01-11 | Raymond W Warren | Fluid pulse width modulation |
| US3325103A (en) * | 1964-08-05 | 1967-06-13 | Aerospace Corp | Thrust vector control for reaction engines |
-
1966
- 1966-03-22 FR FR54510A patent/FR1488272A/fr not_active Expired
-
1967
- 1967-03-16 BE BE695600D patent/BE695600A/xx unknown
- 1967-03-21 DE DE1967B0091700 patent/DE1578081B2/de active Granted
- 1967-03-21 US US624813A patent/US3502288A/en not_active Expired - Lifetime
- 1967-03-21 GB GB03189/67A patent/GB1185193A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE1578081A1 (de) | 1971-09-16 |
| FR1488272A (fr) | 1967-07-13 |
| GB1185193A (en) | 1970-03-25 |
| DE1578081B2 (de) | 1976-07-22 |
| US3502288A (en) | 1970-03-24 |