JPH043299U - - Google Patents
Info
- Publication number
- JPH043299U JPH043299U JP3902090U JP3902090U JPH043299U JP H043299 U JPH043299 U JP H043299U JP 3902090 U JP3902090 U JP 3902090U JP 3902090 U JP3902090 U JP 3902090U JP H043299 U JPH043299 U JP H043299U
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- thrust
- combustion gas
- fixed nozzle
- nozzles
- 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
- 239000000567 combustion gas Substances 0.000 claims 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Nozzles (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1990039020U JP2522167Y2 (ja) | 1990-04-13 | 1990-04-13 | 飛しよう体の推力偏向装置 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1990039020U JP2522167Y2 (ja) | 1990-04-13 | 1990-04-13 | 飛しよう体の推力偏向装置 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH043299U true JPH043299U (th) | 1992-01-13 |
JP2522167Y2 JP2522167Y2 (ja) | 1997-01-08 |
Family
ID=31547545
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1990039020U Expired - Lifetime JP2522167Y2 (ja) | 1990-04-13 | 1990-04-13 | 飛しよう体の推力偏向装置 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2522167Y2 (th) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7108223B2 (en) * | 2002-11-07 | 2006-09-19 | Raytheon Company | Missile control system and method |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59176197A (ja) * | 1982-11-29 | 1984-10-05 | ソシエテ・ナシヨナ−ル・インダストリエル・アエロスパシエ−ル | 横向きのガス状噴流によるミサイル操縦装置 |
JPS62125896U (th) * | 1986-01-31 | 1987-08-10 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4384690A (en) | 1981-03-06 | 1983-05-24 | The United States Of America As Represented By The Secretary Of The Navy | Thrust vector control for large deflection angles |
-
1990
- 1990-04-13 JP JP1990039020U patent/JP2522167Y2/ja not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59176197A (ja) * | 1982-11-29 | 1984-10-05 | ソシエテ・ナシヨナ−ル・インダストリエル・アエロスパシエ−ル | 横向きのガス状噴流によるミサイル操縦装置 |
JPS62125896U (th) * | 1986-01-31 | 1987-08-10 |
Also Published As
Publication number | Publication date |
---|---|
JP2522167Y2 (ja) | 1997-01-08 |