Static Tests of the J97 Powered, External Augmenter V/STOL Wind Tunnel Model
StarBooster Demonstrator Cluster Configuration Analysis/Verification Program
Stability derivatives of triangular wings at supersonic speeds
Stability Derivatives of Low-Aspect-Ratio Triangular Wings at Subsonic and Supersonic Speeds
Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data
Stability control and energy saving for propulsion of a biomimetic autonomous underwater vehicle
Spanwise Wing Loads on the Space Shuttle Orbiter during Roll Maneuver
Spanwise loading for wings and control surfaces of low aspect ratio
Space Transportation Infrastructure Supported By Propellant Depots
Space Shuttle Phase B Wind Tunnel Model and Test Information. Volume 3. Part 2. Launch Configuration
Space Shuttle Phase B Wind Tunnel Model and Test Information. Volume 2: Orbiter Configuration
Space Shuttle Phase B Wind Tunnel Model and Test Information. Volume 2: Orbiter Configuration
Space Shuttle Aerothermodynamics Technology Conference. Volume 3 Aerodynamics
Space Shuttle Aerodynamic Heating Tests of the MDAC delta Wing Orbiter and Canard Booster
Space Shuttle Aerodynamic Characteristics of the Nr delta Wing Orbiter, M Equals 0.6 to 1.3
Spacecraft Thruster Control via Sigma-Delta Modulation
Spacecraft Thruster Control via Sigma-Delta Modulation