DLR Reusability Flight Experiment ReFEx
Cost estimation for launch vehicle families considering uncertain market scenarios
Feasibility of Large Launch Vehicle Recovery
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
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Space Launch System Engine Out Capabilities
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
Lyapunov based PD/PID in model reference adaptive control for satellite launch vehicle systems
Suggestions for a Roadmap towards Becoming a Launch Capable Nation
Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Low cost small-satellite access to space using hybrid rocket propulsion
Synthesizing a New Launch Vehicle Failure Probability Based on Historical Flight Data
An Optimized Trajectory for a Two-Stage, Surface-to-Orbit Titan Launch Vehicle
Ames Modular Common Spacecraft Bus
Robust Space Launcher Control with Time-Varying Objectives
Mission Success of U.S. Launch Vehicle Flights from a Propulsion Stage-Based Perspective: 1980-2015
Menagerie: an Automated Approach to Launch Vehicle Design
Ares Projects: Back to the Future
Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control
Simultaneous Sizing of a Rocket Family with Embedded Trajectory Optimization
Robust adaptive backstepping control for reentry reusable launch vehicles
Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
Adaptive control design for active Pogo suppression based on vibration-acceleration feedback
Launch Vehicles and Launch Operations
Conceptual Design, Feasibility and Payoff Analysis of a Third Stage for EELV
Emerging US Space Launch, Trends and Space Solar Power
Wind-Tunnel to Full-Scale Mapping of Winds and Loads for Launch-Vehicle Ground Wind Loads
Design aspects of launch vehicle sizing including air-breathing propulsion
Launching to the Moon and Beyond
The Design of Bolts Tighting Test System for Launch Vehicle Based on PLC and Servo Motor
Gas Permeation of Composites Subjected to Impact for Cryogenic Applications
Initial Orbit Determination Using Single Frequency GPS Measurements of Launch Vehicle