Title:
ロケットエンジン
Document Type and Number:
Japanese Patent JP4439267
Kind Code:
B2
Abstract:
The rocket motor combustion chamber (1) is constituted by a first monolithic thermo-structural composite material comprising a porous skin (5) through which a part of the fuel is introduced into the heart (C) of the combustion chamber. The combustion chamber is connected by a neck (3) to a divergent pipe (2) through which the exhaust gases pass.
Inventors:
Calabro, Max
Application Number:
JP2003573286A
Publication Date:
March 24, 2010
Filing Date:
February 27, 2003
Export Citation:
Assignee:
EADS SPACE TRANSPORTATION SA
MBDA France
MBDA France
International Classes:
F02K9/00; F02K9/64; F02K9/52; F02K9/97
Domestic Patent References:
| JP2000503094A | ||||
| JP3206345A | ||||
| JP33005356B1 |
Foreign References:
| US3069847 | ||||
| WO2000042310A1 |
Attorney, Agent or Firm:
Shoji Suzue
Toshiyuki Kimura
Toshiyuki Kimura