06705076 is referenced by 1 patents and cites 2 patents.

Thrust chamber housing for a driving mechanism for space travel applications which is fastened to an injection head with its first end and which includes a combustion chamber housing of a highly heat-resistant steel, a nozzle element of a platinum-iridium alloy, and an expansion nozzle housing of a highly heat-resistant steel, whereby the combustion chamber housing is welded through a first intermediate ring with the nozzle element and the nozzle element is welded through a second intermediate ring with the expansion nozzle housing by means of welded connections, whereby the first and the second intermediate ring are made of a platinum-rhodium alloy.

Title
Rocket thrust chamber
Application Number
10/9726
Publication Number
6705076 (B1)
Application Date
December 17, 2001
Publication Date
March 16, 2004
Inventor
Armin Sowa
Ottobrunn
US
Agent
Crowell & Moring
US
Assignee
Astrium
US
IPC
F02K 9/62
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