GB1230760A - - Google Patents
Info
- Publication number
- GB1230760A GB1230760A GB1230760DA GB1230760A GB 1230760 A GB1230760 A GB 1230760A GB 1230760D A GB1230760D A GB 1230760DA GB 1230760 A GB1230760 A GB 1230760A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotation
- rocket
- deflector
- latch
- gyroscope
- Prior art date
- 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
- 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
Abstract
1,230,760. Deflecting propulsion jets. M. L. AVIATION CO. Ltd. 17 June, 1968 [28 April, 1967], No. 19667/67. Heading B7G. In a rocket control system, rotation about the longitudinal axis is effected by fixed fins while a movable deflecting surface at the exhaust nozzle provides an unbalanced lateral force, increasing the rocket pitch angle so as to cause a curved flight path. The deflector 5 is rotatably mounted on ball-race 6 and surrounds the exhaust nozzle 4. It is caused to oscillate, about a predetermined central position by alternate rotation first in one direction by the exhaust gases and rotation in the opposite direction by the rocket rotation. The first rotation is caused by the action of the gases on vanes 12 while the second is effected by engaging the latch 17, 23 with the ring 7, fixed to the rocket body, thereby rotating the deflector with the rocket. The change in roll position of the deflector is sensed by a gyroscope, an output signal from which releases the latch 17, 23 to permit opposite rotation due to the exhaust gases. Following a rotation in that sense the gyroscope relocks the latch.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1966767 | 1967-04-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1230760A true GB1230760A (en) | 1971-05-05 |
Family
ID=10133184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1230760D Expired GB1230760A (en) | 1967-04-28 | 1967-04-28 |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1230760A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4541590A (en) * | 1981-07-24 | 1985-09-17 | The Commonwealth Of Australia | Roll measuring device |
| US4562980A (en) * | 1980-11-14 | 1986-01-07 | The Commonwealth Of Australia | Rocket vehicle |
| EP2261593A1 (en) * | 2009-06-12 | 2010-12-15 | MBDA France | System for controlling the path of a mobile moved by jet propulsion |
-
1967
- 1967-04-28 GB GB1230760D patent/GB1230760A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4562980A (en) * | 1980-11-14 | 1986-01-07 | The Commonwealth Of Australia | Rocket vehicle |
| US4541590A (en) * | 1981-07-24 | 1985-09-17 | The Commonwealth Of Australia | Roll measuring device |
| EP2261593A1 (en) * | 2009-06-12 | 2010-12-15 | MBDA France | System for controlling the path of a mobile moved by jet propulsion |
| WO2010142867A1 (en) * | 2009-06-12 | 2010-12-16 | Mbda France | System for controlling the trajectory of a jet-propelled mobile |
| FR2946741A1 (en) * | 2009-06-12 | 2010-12-17 | Mbda France | SYSTEM FOR CONTROLLING THE TRACK OF A MU MOBILE BY REACTION. |
| RU2484417C1 (en) * | 2009-06-12 | 2013-06-10 | Мбда Франс | Jet moving body path control system |
| US9297623B2 (en) | 2009-06-12 | 2016-03-29 | Mbda France | System for controlling the trajectory of a jet-propelled mobile |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |