Appraisal of Aerodynamics and Aerothermodynamics of RFS and LFBB (LOx/CH4) ESA Future Launchers Preparatory Program Concepts

Author:

Pezzella Giuseppe1,Marini Marco1,Kauffmann Jens2,Dapra Albert3,Tomatis Carlo3

Affiliation:

1. Centro Italiano Ricerche Aerospaziali (CIRA)

2. ESA

3. Next Generation Launcher Prime S.p.A.

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Prabhu, D. K. System Design Constraints-Trajectory Aerothermal Environments. RTO AVT/VKI Lecture Series in Critical Technologies for HypersonicVehicleDevelopment,10-14May2004.

2. Schettino, A.,Pezzella, G., etal USV_X-PhaseA Aerodynamicand Aerothermodynamic Analysis. CIRA-CF-06-1393.

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1. CFD design capabilities for next generation high-speed aircraft;Acta Astronautica;2021-01

2. Launchers: Present and Future;Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles;2015

3. Aerodynamic and aerothermodynamic design of Future Launchers Preparatory Program concepts;Aerospace Science and Technology;2012-12

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