ES186167U - Assembly of exhaustation nozzle for rocket engines. (Machine-translation by Google Translate, not legally binding) - Google Patents
Assembly of exhaustation nozzle for rocket engines. (Machine-translation by Google Translate, not legally binding)Info
- Publication number
- ES186167U ES186167U ES0186167U ES186167U ES186167U ES 186167 U ES186167 U ES 186167U ES 0186167 U ES0186167 U ES 0186167U ES 186167 U ES186167 U ES 186167U ES 186167 U ES186167 U ES 186167U
- Authority
- ES
- Spain
- Prior art keywords
- nozzle
- exhaust
- deviation
- exhaust gases
- translation
- 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.)
- Granted
Links
- 239000007789 gas Substances 0.000 abstract 5
Landscapes
- Exhaust Silencers (AREA)
Abstract
Exhaust nozzle assembly for rocket motors, characterized in that it comprises a low expansion exhaust nozzle provided with a control device of the thrust vector of the rocket motor, comprising at least three deviation elements of the exhaust gases located equiangularly around the nozzle, each deflecting element having a deviation surface of the exhaust gases and each deflection element being provided with a corresponding actuator, for moving the element to a position of a plurality of deviating positions of shape that when the exhaust gas bypass element is in its exhaust deviation position if it is considered in any longitudinal section of the exhaust deviation member, said section containing the longitudinal axis of the nozzle is located radially towards outside the exit end of the nozzle and projects axially beyond said end, so that the deflection surface will react with the exhaust gases exiting the nozzle, to divert said exhaust gases and thereby effect the control of the thrust vector of the engine of rocket. (Machine-translation by Google Translate, not legally binding)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES1972186167U ES186167Y (en) | 1972-11-28 | 1972-11-28 | EXHAUSTATION NOZZLE ASSEMBLY FOR ROCKET ENGINES. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES1972186167U ES186167Y (en) | 1972-11-28 | 1972-11-28 | EXHAUSTATION NOZZLE ASSEMBLY FOR ROCKET ENGINES. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES186167U true ES186167U (en) | 1973-10-16 |
| ES186167Y ES186167Y (en) | 1974-07-01 |
Family
ID=8358006
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES1972186167U Expired ES186167Y (en) | 1972-11-28 | 1972-11-28 | EXHAUSTATION NOZZLE ASSEMBLY FOR ROCKET ENGINES. |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES186167Y (en) |
-
1972
- 1972-11-28 ES ES1972186167U patent/ES186167Y/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| ES186167Y (en) | 1974-07-01 |
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