DLR Reusability Flight Experiment ReFEx
Cost estimation for launch vehicle families considering uncertain market scenarios
Feasibility of Large Launch Vehicle Recovery
Two-Stage Launch Vehicle Trajectory Modeling for Low Earth Orbit Applications
Space Launch System Engine Out Capabilities
An Optimized Trajectory for a Two-Stage, Surface to Orbit Titan Launch Vehicle
Validation of the Corcos Model for the Space Launch System using Unsteady Pressure Sensitive Paint
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Fiber Optic Sensors for Launch Vehicles Project
Space Launch System Engine Out Capabilities
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle
Effect of Initial State of Air-launch on Payload of Launch Vehicle
Ares I–X Flight Test Vehicle similitude to the Ares I Crew Launch Vehicle
New Launchers for Small Satellite Systems
Working RideShare for the U Class Payload