A PROPOSAL OF NEW FUSELAGE CONFIGURATIONS FOR REALIZING REUSABLE LAUNCH VEHICLES
Reduction of Aerodynamic Interference for Separation of Two-Stage Reuseable Launch Vehicles
A Study of Fuselage Configurations for Reusable Launch Vehicles
A Study of Fuselage Effects on Aerodynamic Characteristics of Reusable Launch Vehicles
Lift Augmentation by Lateral Blowing for RLVs with Various Fuselage-Cross Sections