GB329229A - Improvements in rockets - Google Patents
Improvements in rocketsInfo
- Publication number
- GB329229A GB329229A GB2224429A GB2224429A GB329229A GB 329229 A GB329229 A GB 329229A GB 2224429 A GB2224429 A GB 2224429A GB 2224429 A GB2224429 A GB 2224429A GB 329229 A GB329229 A GB 329229A
- Authority
- GB
- United Kingdom
- Prior art keywords
- choke
- rocket
- steel
- propellant material
- curved entrance
- 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
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/68—Line-carrying missiles, e.g. for life-saving
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Abstract
329,229. Spanner, E. F. July 19, 1929. Projectiles. - The choke of a steel-tubed rocket is formed of steel, cast iron, or hard brass and has a discharge orifice with a curved entrance and a substantially parallel throat. In one construction, the choke 2 is screwed in to the rocket tube 1 containing propellant material 3. Since the choke 2, owing to its curved entrance. does not bear against the rear end of the propellant material, the diaphragm 4, made of celluloid or like rigid combustible substance, is shaped as a, complete or truncated cone. Holes 4a mav be provided therein to ensure the firing of the rocket charge,
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2224429A GB329229A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
GB1265330A GB330493A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2224429A GB329229A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
Publications (1)
Publication Number | Publication Date |
---|---|
GB329229A true GB329229A (en) | 1930-05-15 |
Family
ID=10176229
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1265330A Expired GB330493A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
GB2224429A Expired GB329229A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1265330A Expired GB330493A (en) | 1929-07-19 | 1929-07-19 | Improvements in rockets |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB330493A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2944389A (en) * | 1944-11-20 | 1960-07-12 | Clarence E Weinland | Rotating rocket motor and method of making same |
US3137126A (en) * | 1961-01-11 | 1964-06-16 | North American Aviation Inc | Method and means for forming a gaseous passage |
GB2528944A (en) * | 2014-08-06 | 2016-02-10 | John Douglas Michael Wraige | Choke |
CN108955378A (en) * | 2018-07-20 | 2018-12-07 | 航天科工仿真技术有限责任公司 | A kind of bindiny mechanism not generating reaction force and fire extinguisher bomb launching tube device |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2462135A (en) * | 1944-04-06 | 1949-02-22 | Leslie A Skinner | Rocket primer |
FR954765A (en) * | 1946-10-30 | 1950-01-05 | ||
US2627160A (en) * | 1947-04-01 | 1953-02-03 | Macdonald Gilmour Craig | Rocket igniter |
US2613497A (en) * | 1947-04-01 | 1952-10-14 | Macdonald Gilmour Craig | Controllable rocket thrust device |
DE1113612B (en) * | 1957-07-11 | 1961-09-07 | Soc Tech De Rech Ind | Closing body for the nozzle of recoil engines |
-
1929
- 1929-07-19 GB GB1265330A patent/GB330493A/en not_active Expired
- 1929-07-19 GB GB2224429A patent/GB329229A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2944389A (en) * | 1944-11-20 | 1960-07-12 | Clarence E Weinland | Rotating rocket motor and method of making same |
US3137126A (en) * | 1961-01-11 | 1964-06-16 | North American Aviation Inc | Method and means for forming a gaseous passage |
GB2528944A (en) * | 2014-08-06 | 2016-02-10 | John Douglas Michael Wraige | Choke |
CN108955378A (en) * | 2018-07-20 | 2018-12-07 | 航天科工仿真技术有限责任公司 | A kind of bindiny mechanism not generating reaction force and fire extinguisher bomb launching tube device |
Also Published As
Publication number | Publication date |
---|---|
GB330493A (en) | 1930-06-12 |
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