GB910017A - Propulsion means for projectiles - Google Patents
Propulsion means for projectilesInfo
- Publication number
- GB910017A GB910017A GB37202/60A GB3720260A GB910017A GB 910017 A GB910017 A GB 910017A GB 37202/60 A GB37202/60 A GB 37202/60A GB 3720260 A GB3720260 A GB 3720260A GB 910017 A GB910017 A GB 910017A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- nozzle
- self
- propulsion means
- propellent charge
- 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
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/04—Rifle grenades
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Telescopes (AREA)
Abstract
910,017. Self - propelled rifle grenades. ANSTALT FUR DIE ENTWICKLUNG VON ERFINDUNGEN UND GEWERBLICHEN ANWENDUNGEN ENERGA. Oct. 28, 1960 [Nov. 25, 1959], No. 37202/60. Classes 9 (1) and 9 (2). A self-propulsion means for a rifle grenade comprises a combustion chamber 2 containing a propellent charge 3, a Venturi-nozzle 4 placed in the rear of the chamber and a tail tube 5. At the fore part of the nozzle are radial cavities 6 separated by partitions 7, the latter being cut-away as at 10 thereby forming shoulders on which the propellent charge rests and is centred within the chamber. The Venturinozzle 4 is rigidly held in position by having its peripheral rim 15 forced against a peripheral shoulder 14 of the chamber 2 by the screwing of tail 5 into the rear of the chamber.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH8104159 | 1959-11-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB910017A true GB910017A (en) | 1962-11-07 |
Family
ID=4538454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB37202/60A Expired GB910017A (en) | 1959-11-25 | 1960-10-28 | Propulsion means for projectiles |
Country Status (5)
| Country | Link |
|---|---|
| CH (1) | CH359627A (en) |
| DE (1) | DE1162725B (en) |
| FR (1) | FR1274683A (en) |
| GB (1) | GB910017A (en) |
| NL (1) | NL257331A (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2519905A (en) * | 1945-05-17 | 1950-08-22 | Clarence N Hickman | Driver rocket |
| FR1191494A (en) * | 1959-01-13 | 1959-10-20 | Soc Tech De Rech Ind | Rocket refinements |
| FR1077082A (en) * | 1959-03-10 | 1954-11-04 | Soc Tech De Rech Ind | Rocket safety device |
-
0
- NL NL257331D patent/NL257331A/xx unknown
-
1959
- 1959-11-25 CH CH359627D patent/CH359627A/en unknown
-
1960
- 1960-09-23 FR FR839395A patent/FR1274683A/en not_active Expired
- 1960-09-26 DE DEA35671A patent/DE1162725B/en active Pending
- 1960-10-28 GB GB37202/60A patent/GB910017A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1274683A (en) | 1961-10-27 |
| NL257331A (en) | |
| CH359627A (en) | 1962-01-15 |
| DE1162725B (en) | 1964-02-06 |
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