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title: AIAA international space planes and hypersonic systems and technologies conference
Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow (AIAA 2014-3088)
Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow
Validation of a Leak-free C/SiC Heat Exchanger Technology
Vacuum Ultraviolet Emission Spectroscopy System for Superorbital Re-entries
VACUUM ULTRAVIOLET EMISSION SPECTROSCOPY SYSTEM FOR SUPERORBITAL RE-ENTRIES
USV Status 2011: New Steps Ahead
USV Status 2011: New Steps Ahead
USV Mission - Use of Direct TM/TC Link via European Data Relay Satellite ARTEMIS
USV FLYING TEST BEDS FOR FUTURE GENERATIONS LV TECHNOLOGY DEVELOPMENT
US National Center for Hypersonic Combined Cycle Propulsion: An Overview
US National Center for Hypersonic Combined Cycle Propulsion - An Overview
Using the Vorticity Flux Equations to Model Hypersonic Transition
Using the Vorticity Flux Equations to Model Hypersonic Transition
Use of Temperature Sensitive Paint in the AEDC Hypervelocity Wind Tunnel 9
Use of GNSS Signals to Reconstruct the Shape of the Plasma Sheet Surrounding the Re-Entry Vehicles
Use of an air liquefaction cycle in combined propulsions of advanced space transportation systems
US Army Hypersonic Scramjet Propelled Missile Technology Program
U.S. Air Force space operations vehicle
U. S. Air Force Space Operations Vehicle
Usage of Catalytic Processes in Advanced Power Plants of Hydrocarbon-Fueled Hypersonic Vehicles
Usage of catalytic processes in advanced power plants of hydrocarbon-fueled hypersonic vehicles