Weight Analysis of Two-Stage-To-Orbit Reusable Launch Vehicles for Military Applications
Expendable Second Stage Reusable Space Shuttle Booster. Volume 5 Operations and Resources
We Must Take the Next Steps Towards Safe, Routine Space Travel
Real-Time Sensor Validation System Developed for Reusable Launch Vehicle Testbed
ExFiT Flight Design and Structural Modeling for FalconLAUNCH VIII Sounding Rocket
Simulation and Analyses of Stage Separation Two-Stage Reusable Launch Vehicles
Simulation and Analyses of Staging Maneuvers of Next Generation Reusable Launch Vehicles
Space Transportation Systems Technologies
X-34 Vehicle Aerodynamic Characteristics
Lightcraft Propulsion Technology for Low Cost Access to Space
Structural Sizing of a 25,000-lb Payload, Air-Breathing Launch Vehicle for Single-Stage-to-Orbit
Strategy for Integrating a Large Finite Element Model Using MSC NASTRAN/PATRAN: X-33 Lessons Learned
Advanced Guidance and Control Methods for Reusable Launch Vehicles: Test Results