TY - GEN
T1 - Study of an airbreathing variable cycle engine
AU - Vyvey, Peter
AU - Bosschaerts, Walter
AU - Villace, Victor Fernandez
AU - Paniagua, Guillermo
PY - 2011
Y1 - 2011
N2 - This paper describes the simulation of the Revolutionary Turbine Accelerator in the software EcosimPro. The Revolutionary Turbine Accelerator is a Variable Cycle Engine developed by NASA and General Electric in frame of the Next Generation Launch Technology program. A first simulation was done in EcosimPro by the Von Karman Institude; this paper in particular describes a simulation done using libraries from the European Space and Propulsion System Simulation. Results of the simulation are described and compared to results from the first simulation. Based on these results, a weight analysis of the Revolutionary Turbine Accelerator was performed.
AB - This paper describes the simulation of the Revolutionary Turbine Accelerator in the software EcosimPro. The Revolutionary Turbine Accelerator is a Variable Cycle Engine developed by NASA and General Electric in frame of the Next Generation Launch Technology program. A first simulation was done in EcosimPro by the Von Karman Institude; this paper in particular describes a simulation done using libraries from the European Space and Propulsion System Simulation. Results of the simulation are described and compared to results from the first simulation. Based on these results, a weight analysis of the Revolutionary Turbine Accelerator was performed.
UR - https://www.scopus.com/pages/publications/84880677994
M3 - Conference contribution
AN - SCOPUS:84880677994
SN - 9781600869495
T3 - 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
BT - 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
T2 - 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
Y2 - 31 July 2011 through 3 August 2011
ER -