DLR Reusability Flight Experiment ReFEx
Cost estimation for launch vehicle families considering uncertain market scenarios
Two-Stage Launch Vehicle Trajectory Modeling for Low Earth Orbit Applications
Feasibility of Large Launch Vehicle Recovery
Space Launch System Engine Out Capabilities
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
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
Fiber Optic Sensors for Launch Vehicles Project
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
Working RideShare for the U Class Payload
New Launchers for Small Satellite Systems
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle