Computer Science – Performance
Scientific paper
Jan 2002
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002iaf..confe.789i&link_type=abstract
IAF abstracts, 34th COSPAR Scientific Assembly, The Second World Space Congress, held 10-19 October, 2002 in Houston, TX, USA.,
Computer Science
Performance
Scientific paper
At Astrium (former DaimlerChrysler Aerospace Dasa) technology developments for thrust chambers of future launch vehicle rocket engines are presently being performed within the frame of German national technology programs sponsored by the German Aerospace Center. The main focus of these technology developments is on thrust chamber technologies for future, reusable or semi-reusable high performance launch vehicle liquid rocket engines. This paper shows the present status and the results of the following thrust chamber technologies investigated experimentally on subscale chamber level: - Development of technologies for increased heat transfer to the thrust chamber wall for - Developments of thermal barrier coatings for the thrust chamber hot gas wall for - For future staged combustion cycle engines a subscale chamber program with a new
Alting Jan
Immich Hans
Kretschmer Joachim
Preclik Dieter
No associations
LandOfFree
Technologies for Thrust Chambers of Future Launch Vehicle Liquid Rocket Engines does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Technologies for Thrust Chambers of Future Launch Vehicle Liquid Rocket Engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Technologies for Thrust Chambers of Future Launch Vehicle Liquid Rocket Engines will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1332770