JPS529708A - Injector for rocket engine - Google Patents
Injector for rocket engineInfo
- Publication number
- JPS529708A JPS529708A JP8641175A JP8641175A JPS529708A JP S529708 A JPS529708 A JP S529708A JP 8641175 A JP8641175 A JP 8641175A JP 8641175 A JP8641175 A JP 8641175A JP S529708 A JPS529708 A JP S529708A
- Authority
- JP
- Japan
- Prior art keywords
- injector
- rocket engine
- fuel
- oxidant
- high pressure
- 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.)
- Pending
Links
Abstract
PURPOSE: To facilitate atomization of oxidant and fuel in combustion chamber without oxidizing agent or fuel pump of high pressure or large size, by providing oscillation device in injector.
COPYRIGHT: (C)1977,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8641175A JPS529708A (en) | 1975-07-14 | 1975-07-14 | Injector for rocket engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8641175A JPS529708A (en) | 1975-07-14 | 1975-07-14 | Injector for rocket engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS529708A true JPS529708A (en) | 1977-01-25 |
Family
ID=13886114
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8641175A Pending JPS529708A (en) | 1975-07-14 | 1975-07-14 | Injector for rocket engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS529708A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5265415A (en) * | 1993-01-27 | 1993-11-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Liquid fuel injection elements for rocket engines |
-
1975
- 1975-07-14 JP JP8641175A patent/JPS529708A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5265415A (en) * | 1993-01-27 | 1993-11-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Liquid fuel injection elements for rocket engines |
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