GB759350A - Improvements in and relating to blast tubes - Google Patents
Improvements in and relating to blast tubesInfo
- Publication number
- GB759350A GB759350A GB3341053A GB3341053A GB759350A GB 759350 A GB759350 A GB 759350A GB 3341053 A GB3341053 A GB 3341053A GB 3341053 A GB3341053 A GB 3341053A GB 759350 A GB759350 A GB 759350A
- Authority
- GB
- United Kingdom
- Prior art keywords
- relating
- tube
- blast tubes
- durestos
- throat
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- linings; Ablative coatings
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Insulating Bodies (AREA)
- Insulators (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
759.350. Jet propulsion nozzles. ENGLISH ELECTRIC CO., Ltd. Nov. 26, 1954 [Dec. 1, 1953], No. 33410/53. Drawings to Specification. Class 110(3) [Also in Group XII] In a rocket blast tube, an inner tubular core consisting of the heat venting and insulating material "Durestos" is surrounded by a wrapping of glass tape which is bonded into position by a polyester resin. The tube has a venturi section, the throat of which has a carbon insert.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3341053A GB759350A (en) | 1953-12-01 | 1953-12-01 | Improvements in and relating to blast tubes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3341053A GB759350A (en) | 1953-12-01 | 1953-12-01 | Improvements in and relating to blast tubes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB759350A true GB759350A (en) | 1956-10-17 |
Family
ID=10352592
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3341053A Expired GB759350A (en) | 1953-12-01 | 1953-12-01 | Improvements in and relating to blast tubes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB759350A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1102013B (en) * | 1958-01-08 | 1961-03-09 | Ici Ltd | rocket |
DE1129022B (en) * | 1958-01-07 | 1962-05-03 | Ici Ltd | Expansion cone nozzle for jet engines |
DE1133948B (en) * | 1954-12-22 | 1962-07-26 | Ici Ltd | Jet engine housing, in particular rocket housing |
DE1214476B (en) * | 1956-12-21 | 1966-04-14 | Haveg Industries Inc | High-temperature-resistant construction or protective layer material for rocket combustion chambers or missile outer shells |
DE1235675B (en) * | 1962-01-29 | 1967-03-02 | Thiokol Chemical Corp | Combustion chamber and nozzle for a rocket engine |
FR2316057A1 (en) * | 1975-06-09 | 1977-01-28 | Imp Metal Ind Kynoch Ltd | Gas pipe for rocket motor - produced from parts and simultaneously given plastic protective lining |
US4404887A (en) * | 1980-06-23 | 1983-09-20 | General Dynamics, Pomona Division | Recoil reducer |
-
1953
- 1953-12-01 GB GB3341053A patent/GB759350A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1133948B (en) * | 1954-12-22 | 1962-07-26 | Ici Ltd | Jet engine housing, in particular rocket housing |
DE1214476B (en) * | 1956-12-21 | 1966-04-14 | Haveg Industries Inc | High-temperature-resistant construction or protective layer material for rocket combustion chambers or missile outer shells |
DE1129022B (en) * | 1958-01-07 | 1962-05-03 | Ici Ltd | Expansion cone nozzle for jet engines |
DE1102013B (en) * | 1958-01-08 | 1961-03-09 | Ici Ltd | rocket |
DE1235675B (en) * | 1962-01-29 | 1967-03-02 | Thiokol Chemical Corp | Combustion chamber and nozzle for a rocket engine |
FR2316057A1 (en) * | 1975-06-09 | 1977-01-28 | Imp Metal Ind Kynoch Ltd | Gas pipe for rocket motor - produced from parts and simultaneously given plastic protective lining |
US4404887A (en) * | 1980-06-23 | 1983-09-20 | General Dynamics, Pomona Division | Recoil reducer |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB759350A (en) | Improvements in and relating to blast tubes | |
GB2012370B (en) | Air intake for supersonic air breathing jet propulsion engines | |
SE302660B (en) | ||
GB900040A (en) | Exhaust nozzle with thrust deflector | |
SE7902056L (en) | DEVICE FOR GENERATION OF AN ELECTRICALLY CHARGED GAS RAY | |
JPS52154921A (en) | Fuel jet apparatus | |
GB887036A (en) | Apparatus for making fibres from thermoplastic materials, particularly glass fibres | |
JPS5362032A (en) | Carburetter with compensating air passage | |
GB750417A (en) | Improvements in or relating to pitot tube devices | |
CA473317A (en) | Deflecting fuel jets towards a region of turbulence in propulsive gaseous streams | |
JPS53134189A (en) | Nuclear fuel element | |
ES257435A1 (en) | Gaseous fuel burner of low deflagration speed (Machine-translation by Google Translate, not legally binding) | |
CA480788A (en) | Jet propulsion and control means therefor | |
CA500396A (en) | Jet propulsion and gas turbine engine operation and fuel thereof | |
GB970658A (en) | Improved liquid atomizing device | |
GB1049486A (en) | Flow regulating devices | |
JPS531346A (en) | High frequency heater | |
CA653306A (en) | Gas turbine jet propulsion engine units for aircraft and also jet propelled aircraft | |
JPS5358207A (en) | Magnetic tape feeder | |
GB754038A (en) | Pulse jet unit with leak gas deflecting device | |
FR1233416A (en) | Improvements made to rocket-type jet engines, in particular for model aircraft | |
CA527350A (en) | Flying machines having a propelling power plant with an air intake | |
GB1399886A (en) | Inflatable bung | |
AU259847B2 (en) | Improvements in means for heating a stream of air or other gas | |
CA480789A (en) | Jet propulsion and control means therefor |