3D Carbon-Carbon Composites are Revolutionizing Upper Stage Liquid Rocket Engine Performance by Allowing Introduction of Large Nozzle Extension

Author(s):  
Alain Lacombe ◽  
Thierry Pichon ◽  
Marc Lacoste
2019 ◽  
Vol 11 (3) ◽  
pp. 135-145 ◽  
Author(s):  
Alexandru-Iulian ONEL ◽  
Oana-Iuliana POPESCU ◽  
Ana-Maria NECULAESCU ◽  
Tudorel-Petronel AFILIPOAE ◽  
Teodor-Viorel CHELARU

The paper presents a fast mathematical model that can be used to quickly asses the propulsive characteristics of liquid propelled rocket engines. The main propulsive parameters are computed using combustion surfaces obtained after a nonlinear data fitting analysis. This approach is much more time efficient than using standard codes which rely on frequent calls of the Fuel Combustion Charts and interpolating their data. The tool developed based on the proposed mathematical model can be used separately or it can be integrated in a multidisciplinary optimisation algorithm for a preliminary microlauncher design.


2010 ◽  
Vol 34 (4) ◽  
pp. 443-448
Author(s):  
Won-Kook Cho ◽  
Soon-Young Park ◽  
Chang-Ho Nam ◽  
Chul-Woong Kim

1997 ◽  
Author(s):  
R. Ellis ◽  
J. Lee ◽  
F. Payne ◽  
M. Lacoste ◽  
A. Lacombe ◽  
...  

2020 ◽  
Vol 57 (2) ◽  
pp. 391-397
Author(s):  
S. B. Verma ◽  
Oskar Haidn

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