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50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
757 NLF (Natural Laminar Flow) Glove Flight Test Results
1982 AFOSR/AFRPL Rocket Propulsion Research Meeting Held at Lancaster, California on 2-4 March 1982
1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 2 Part 1
2008 Stability, Security, Transition and Reconstruction Operations Conference
AAS/GSFC 13th International Symposium on Space Flight Dynamics, Volume 2
Abort Separation Study of a Shuttle Orbiter and External Tank at Hypersonic Speeds
A Brushless DC Torquer-Driven Reaction Wheel for Spacecraft Attitude Control
Absolute Stability Analysis of Attitude Control Systems for Large Boosters
A Calculation of the Lateral Hunting Motion of a Tracked Vehicle
A Calculation of the Profile Drag of Airfoils at Low Mach Numbers
Accident Avoidance Capabilities of Mopeds. Volume I: Executve Summary
Accident Avoidance Capabilities of Mopeds. Volume II: Technical Report
Accurate and Efficient Vortex-Capturing for Rotor Blade Vortex Interaction
Achieving Adequate United States Maritime Capital in an Era of Declining Resources
A Comment on a Critical Case of the Stability of a Singular Point on a Plane
A Comparison and Evaluation of Two Methods of Extracting Stability Derivatives from Flight Test Data
A Comparison of in-Flight and Ground Based Pitch Attitude Tracking Experiments
A Contribution to Stabilization of Flight Vehicle Parachute Systems
A Contribution to the Study of the Use of 1-Phenyl-3-Pyrazolidone as a Developing Agent
Acoustic Analysis and Design of the E-STA MSA Simulator
Acoustic Liner Feasibility Program Final Report, 19 Nov. 1968 - 19 Apr. 1970
Active Flexible Wing Aeroservoelastic Wind-Tunnel Test Program
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Active Suppression of Aeroelastic Instabilities for Forward Swept Wings
Actuator placement for active sound and vibration control