Title:
エンジンノズル内に案内翼を有するロケットエンジン
Document Type and Number:
Japanese Patent JP2007506905
Kind Code:
A
Abstract:
A rocket engine having guide vanes in the engine nozzle the guide vanes (2) being mounted for turning at or near the rearmost ends of fixed vanes (1) being parallel to the axis of the nozzle and protruding into the combustion chamber of the engine. The foremost ends (4) of the guide vanes (2) may be shielded by the rearmost ends of the fixed vanes (1), and the guide vanes (2) may be individually turnable.
Inventors:
Obeck, Oland
Application Number:
JP2006527932A
Publication Date:
March 22, 2007
Filing Date:
September 14, 2004
Export Citation:
Assignee:
NAMMO RAUFOSS AS
International Classes:
F02K9/90; F02K9/84; F02K9/88
Domestic Patent References:
| JP2002227723A | 2002-08-14 | |||
| JP2001018897A | 2001-01-23 |
Foreign References:
| US5078336A | 1992-01-07 | |||
| US3743184A | 1973-07-03 | |||
| US6450443B1 | 2002-09-17 | |||
| US5511745A | 1996-04-30 | |||
| US3260205A | 1966-07-12 |
Attorney, Agent or Firm:
Shohei Oguri
Hironori Honda
Toshimitsu Ichikawa
Takeshi Takamatsu
Hironori Honda
Toshimitsu Ichikawa
Takeshi Takamatsu