GB773190A - Improvements relating to missiles and like bodies - Google Patents
Improvements relating to missiles and like bodiesInfo
- Publication number
- GB773190A GB773190A GB1993152A GB1993152A GB773190A GB 773190 A GB773190 A GB 773190A GB 1993152 A GB1993152 A GB 1993152A GB 1993152 A GB1993152 A GB 1993152A GB 773190 A GB773190 A GB 773190A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missile
- parts
- charge
- gun
- aug
- 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
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
773,190. Self-propelled missile ; ammunition. BLACKER, L. V. S. Aug. 7, 1953 [Aug. 7, 1952], No. 19931/52. Classes 9 (1) and 9 (2). A self-propelled missile, Fig. 2, having an explosive charge 8 with a nose fuze 20, a propellent 10 the combustion products from which discharge, through the nozzles 12 and a launching charge 9, is fired by fitting the tube 4 over the spigot rod in the gun (not shown). The charge 9 is ignited by the spigot and simultaneously ejects the missile from the gun and ignites 10 through the passages 11. The centre lines of the nozzles 12 converge to a point on the missile longitudinal axis to the rear of the centre of gravity. In a further embodiment, Fig. 8, the missile is formed of two parts 34, 36 connected by a flexible rod 38. The propellant 42 discharges through the annular passage 40 and an uneven discharge will cause the parts to move relatively to so adjust the annulus as to produce a balanced thrust. In a further embodiment, not shown, the two parts are connected by a ball and socket joint and the propellent container is caused to rotate relative to the explosive head by means of a system of inclined vanes. Specification 772,651 and 774,786 are referred to in the first Provisional Specification.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1993152A GB773190A (en) | 1952-08-07 | 1952-08-07 | Improvements relating to missiles and like bodies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1993152A GB773190A (en) | 1952-08-07 | 1952-08-07 | Improvements relating to missiles and like bodies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB773190A true GB773190A (en) | 1957-04-24 |
Family
ID=10137525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1993152A Expired GB773190A (en) | 1952-08-07 | 1952-08-07 | Improvements relating to missiles and like bodies |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB773190A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3093964A (en) * | 1960-12-14 | 1963-06-18 | United Aircraft Corp | Two-stage rocket |
| DE1172156B (en) * | 1959-04-23 | 1964-06-11 | Boelkow Entwicklungen Kg | Aerodynamically steerable, recoil-propelled flying body |
| DE1201690B (en) * | 1963-06-04 | 1965-09-23 | Andre Remy Moynet | Twin-engine airplane |
| ITVR20130268A1 (en) * | 2013-12-04 | 2015-06-05 | M G R S R L | JET ENGINE WITH CONFORMED RING NOZZLE FOR SEMIAUTOPROPULSA RIFLE BOMBS AS WELL AS BI-PLURI MISSILES AND STADIUM ROCKERS OF ARTILLERY OR PLURISTADIUM ARTILLERY PROJECTS WITH CORRECTION OF THE TRAJECTORY WITH ADDITIONAL PROJECT, RAZZ |
-
1952
- 1952-08-07 GB GB1993152A patent/GB773190A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1172156B (en) * | 1959-04-23 | 1964-06-11 | Boelkow Entwicklungen Kg | Aerodynamically steerable, recoil-propelled flying body |
| US3093964A (en) * | 1960-12-14 | 1963-06-18 | United Aircraft Corp | Two-stage rocket |
| DE1201690B (en) * | 1963-06-04 | 1965-09-23 | Andre Remy Moynet | Twin-engine airplane |
| ITVR20130268A1 (en) * | 2013-12-04 | 2015-06-05 | M G R S R L | JET ENGINE WITH CONFORMED RING NOZZLE FOR SEMIAUTOPROPULSA RIFLE BOMBS AS WELL AS BI-PLURI MISSILES AND STADIUM ROCKERS OF ARTILLERY OR PLURISTADIUM ARTILLERY PROJECTS WITH CORRECTION OF THE TRAJECTORY WITH ADDITIONAL PROJECT, RAZZ |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2426239A (en) | Rocket shell | |
| US2657630A (en) | Projectile | |
| US2884859A (en) | Rocket projectile | |
| US2989922A (en) | Ramjet propulsion device | |
| US3167016A (en) | Rocket propelled missile | |
| US2206057A (en) | Rocket projectile | |
| GB945409A (en) | Deployable fin assemblies for self-propelled projectiles | |
| US2424934A (en) | Projectile | |
| US3044255A (en) | Powder propulsive for rockets or other self-propelled projectiles | |
| US3024729A (en) | Ram jet projectile | |
| US2504648A (en) | Projectile | |
| US2440271A (en) | Rocket projectile | |
| GB1465550A (en) | Projectile launching device | |
| GB773190A (en) | Improvements relating to missiles and like bodies | |
| US3903802A (en) | Shell construction sealing washer | |
| US2683415A (en) | Rocket motor | |
| US3289587A (en) | Fin stabilized projectile | |
| GB1321588A (en) | Spinstabilised rocket-propelled projectile | |
| US3610093A (en) | Recoilless gun | |
| US2935946A (en) | Telescoping ram jet construction | |
| US2899898A (en) | Auxilliary carriage arrangement for a missile | |
| GB855592A (en) | Improvements in or relating to rocket missiles | |
| FR2260078A1 (en) | Auxiliary charge for rocket launcher - has partition forming chamber ahead of launching member for extra acceleration | |
| GB1120391A (en) | Improvements in or relating to rocketwise propelled projectiles | |
| GB714747A (en) | Improvements in projectiles containing an explosive in the form of a hollow charge |