Powerful & Flexible Future Launchers in 2- or 3-stage Configuration

3STO Three-Stage-To-Orbit AOA Angle of Attack CAD Computer Aided Design DOF Degree of Freedom DRL Down-Range Landing site ELV Expendable Launch Vehicle GLOW Gross Lift-Off Mass IAC In-Air-Capturing LCH4 Liquid Methane LEO Low Earth Orbit LFBB Liquid Fly-Back Booster LH2 Liquid Hydrogen LOX Liquid Oxygen MECO Main Engine Cut Off MR Mixture Ratio RCS Reaction Control System RLV Reusable Launch Vehicle RTLS Return To Launch Site TPS Thermal Protection System TRL Technology Readiness Level TSTO Two-Stage-To-Orbit TVC Thrust Vector Control VTHL Vertical Take-off and Horizontal Landing CoG center of gravity cop center of pressure