Dennis Porrmann

发表

Program AHRES and its Contribution to Assess Features and Current Limitations of Hybrid Rocket Propulsion

Ognjan Bozic, Dennis Porrmann, Daniel Lancelle, 2012 .

REGRESSION RATE MODELS VERSUS EXPERIMENTAL RESULTS FOR HYBRID ROCKET ENGINES BASED ON H2O2 AND HTPB/AL

Stefan May, Ognjan Bozic, Dennis Porrmann, 2013 .

Experimental Evaluation of a High Test Peroxide Catalyst Chamber for a Hybrid Rocket Engine

Stefan May, Ognjan Bozic, Dennis Porrmann, 2013 .

Enhanced development of a catalyst chamber for the decomposition of up to 1.0 kg/s hydrogen peroxide

Stefan May, Dennis Porrmann, Daniel Lancelle, 2016 .

An Advanced Hybrid Rocket Engine for an Alternative Upper Stage of the Brasilian VLM 1 LEO Launcher

Ognjan Bozic, Dennis Porrmann, Georg Poppe, 2014 .

THE LAST ACHIEVEMENTS IN THE DEVELOPMENT OF A ROCKET GRADE HYDROGEN PEROXIDE CATALYST CHAMBER WITH FLOW CAPACITY OF 1 KG/S

Stefan May, Ognjan Bozic, Dennis Porrmann, 2014 .

Analysis of the Ariane 62/64 and Vega-C launcher family

Ognjan Bozic, Josef Klevanski, Etienne Dumont, 2016 .

Estimation of Flow Field Properties and Thrust Performances of Axisymmetric Plug - Nozzles using CFD Simulations

Ognjan Bozic, Dennis Porrmann, 2009 .