GB632637A - Improvements in or relating to jet motors, propellants for use therein and methods of producing hot gases for the purpose of jet propulsion - Google Patents
Improvements in or relating to jet motors, propellants for use therein and methods of producing hot gases for the purpose of jet propulsionInfo
- Publication number
- GB632637A GB632637A GB16034/45A GB1603445A GB632637A GB 632637 A GB632637 A GB 632637A GB 16034/45 A GB16034/45 A GB 16034/45A GB 1603445 A GB1603445 A GB 1603445A GB 632637 A GB632637 A GB 632637A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- propellants
- relating
- fuel
- methods
- 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/425—Propellants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
A fuel for jet-propulsion comprises nitromethane or a mixture of nitromethane and nitroethane. The fuel may also contain promoters of ignition or combustion such as methyl nitrate, ethyl nitrate or methyl oxide. Fluid oxidizing agents such as oxygen may be injected simultaneously with the fuel into the combustion chamber. The Specification as open to inspection under Sect. 91 refers to jet-propulsion fuels comprising other liquid nitroparaffins, particularly such nitroparaffins containing at least 42.6 per cent by weight of oxygen. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US632637XA | 1944-03-11 | 1944-03-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB632637A true GB632637A (en) | 1949-11-28 |
Family
ID=22048050
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16034/45A Expired GB632637A (en) | 1944-03-11 | 1945-06-22 | Improvements in or relating to jet motors, propellants for use therein and methods of producing hot gases for the purpose of jet propulsion |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB632637A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2229176A (en) * | 1983-03-04 | 1990-09-19 | Rheinmetall Gmbh | Liquid propellants |
-
1945
- 1945-06-22 GB GB16034/45A patent/GB632637A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2229176A (en) * | 1983-03-04 | 1990-09-19 | Rheinmetall Gmbh | Liquid propellants |
GB2229176B (en) * | 1983-03-04 | 1991-01-09 | Rheinmetall Gmbh | Liquid propellants. |
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