GB953080A - Improvements in or relating to rocketwise propelled projectiles of the unguided type - Google Patents
Improvements in or relating to rocketwise propelled projectiles of the unguided typeInfo
- Publication number
- GB953080A GB953080A GB2402457A GB2402457A GB953080A GB 953080 A GB953080 A GB 953080A GB 2402457 A GB2402457 A GB 2402457A GB 2402457 A GB2402457 A GB 2402457A GB 953080 A GB953080 A GB 953080A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzles
- rocket
- propelled
- rocketwise
- unguided
- 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
-
- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Testing Of Engines (AREA)
Abstract
953,080. Self-propelled missiles. MINISTER OF AVIATION. July 1, 1958 [July 29, 1957], No. 24024/57. Heading F3A. A rocket projectile is propelled by two concentric charges, the outer of which is the booster charge which provides the rocket with sufficient acceleration to reach a predetermined velocity, while the inner charge burns at a rate sufficient to maintain that velocity. The booster charge is coated with inhibitor at its outer surface and end edges so as to burn over the whole of the inner tubular face, and the combustion gases pass along the annular space between the charges to a ring of nozzles. The inner charge burns only at the rear end and discharges through a single nozzle centrally situated within the first ring of nozzles. The outer nozzles may be inclined to spin the rocket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2402457A GB953080A (en) | 1957-07-29 | 1957-07-29 | Improvements in or relating to rocketwise propelled projectiles of the unguided type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2402457A GB953080A (en) | 1957-07-29 | 1957-07-29 | Improvements in or relating to rocketwise propelled projectiles of the unguided type |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB953080A true GB953080A (en) | 1964-03-25 |
Family
ID=10205169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2402457A Expired GB953080A (en) | 1957-07-29 | 1957-07-29 | Improvements in or relating to rocketwise propelled projectiles of the unguided type |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB953080A (en) |
-
1957
- 1957-07-29 GB GB2402457A patent/GB953080A/en not_active Expired
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