Title:
ロケットエンジン部材並びにロケットエンジン部材の製造方法
Document Type and Number:
Japanese Patent JP4019217
Kind Code:
B2
Abstract:
Method and arrangement for providing a liquid fuel rocket engine member (10). The member has a load bearing wall structure (14) having a plurality of cooling channels (11). For improving the heat transfer, a material with a higher thermal conductivity than the load bearing wall structure (14) is applied to the wall structure.
Inventors:
Hegunder, Yang
Boman, Arne
Boman, Arne
Application Number:
JP2002556492A
Publication Date:
December 12, 2007
Filing Date:
January 09, 2002
Export Citation:
Assignee:
Volvo Aero Corporation
International Classes:
F02K1/00; F02K9/64; B22F3/105; F02K9/97
Domestic Patent References:
| JP4301168A | ||||
| JP8210184A |
Attorney, Agent or Firm:
Kazuo Shigenobu
Hideo Shimizu
Yuichi Takagi
Hideo Shimizu
Yuichi Takagi