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
Validation of the Corcos Model for the Space Launch System using Unsteady Pressure Sensitive Paint
An Optimized Trajectory for a Two-Stage, Surface to Orbit Titan Launch Vehicle
Space Launch System Engine Out Capabilities
Fiber Optic Sensors for Launch Vehicles Project
New Launchers for Small Satellite Systems
Effect of Initial State of Air-launch on Payload of Launch Vehicle
Working RideShare for the U Class Payload
Ares I–X Flight Test Vehicle similitude to the Ares I Crew Launch Vehicle
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle
Lyapunov based PD/PID in model reference adaptive control for satellite launch vehicle systems
Convex optimization of launch vehicle ascent trajectory with heat-flux and splash-down constraints
Convex Optimization of Launch Vehicle Ascent Trajectory with Heat-Flux and Splash-Down Constraints
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Suggestions for a Roadmap towards Becoming a Launch Capable Nation
Low cost small-satellite access to space using hybrid rocket propulsion
Robust Space Launcher Control with Time-Varying Objectives
Synthesizing a New Launch Vehicle Failure Probability Based on Historical Flight Data
Ames Modular Common Spacecraft Bus
Mission Success of U.S. Launch Vehicle Flights from a Propulsion Stage-Based Perspective: 1980-2015
Simultaneous Sizing of a Rocket Family with Embedded Trajectory Optimization
Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control
Menagerie: an Automated Approach to Launch Vehicle Design
Ares Projects: Back to the Future
Robust adaptive backstepping control for reentry reusable launch vehicles
Adaptive control design for active Pogo suppression based on vibration-acceleration feedback
Genetic algorithm based parameter tuning for robust control of launch vehicle in atmospheric flight
Conceptual Design, Feasibility and Payoff Analysis of a Third Stage for EELV
Launch Vehicles and Launch Operations
Launching to the Moon and Beyond
Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
Gas Permeation of Composites Subjected to Impact for Cryogenic Applications
Emerging US Space Launch, Trends and Space Solar Power
Design aspects of launch vehicle sizing including air-breathing propulsion