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ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST CHAMBER DESIGN
ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST CHAMBER DESIGN · Figures and Tables from this paper · One Citation · References.
In this work, we have proposed the novel fuel design concept in order to realize the low emission and combustion control in engine systems. In this concept, we ...
Advancement of Rocket Engine Performance through Novel Approaches for Thrust Chamber Design. Jan 2017. M Ortelt; H Hald; S Michaelides; H Seiler; G Herdrich.
by M Ortelt2017Cited by 1ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST ... cooled rocket thrust chamber, rocket thrust chamber, rocket injector.
by M Ortelt2017Cited by 1ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR ... matrix composites (CMC) has led to novel approaches for designing thrust chambers.

by H Houhou2020Cited by 1Design of the thrust chamber: dimensional analysis of the combustion chamber and the nozzle of rocket engine using LOX/LCH4 propellants.
by M Ortelt2013Cited by 18ceramic combustion chamber section, a new injector design based on porous ... rocket thrust chambers at DLR is structurally affected in general by the ...
15 pages·8 MB
1995Aeronautics
Applications in Rocket Propulsion , Part 1 Jul . ... COMBUSTION AND RADIATION IN OMV THRUST CHAMBER c25 M. G. Giridharan ( CFD Research Corp. , Huntsville ...
Maximum rocket performance is obtained by maximizing thrust chamber temperature for a given propellant. Reactor exit gas maximum temperatures are therefore ...
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