Collection of test data for lateral control with full-span flaps
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Decoupler pylon: wing/store flutter suppressor
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
Directional solar absorptance measurements
Dissociation of the visual placing response into elicited and guided components.
Effect of Lateral Shift of Center of Gravity on Rudder Deflection Required for Trim
Effects of the supersonic transport on the air traffic control system
Environmental Control System /ECS/ space radiator fabrication
Evolution of Autonomous Self-Righting Behaviors for Articulated Nanorovers
Extensions to the Galileo Attitude Control System for the Probe Mission
Flow Physics Study of Sweeping Jet Actuation on a NACA 0015 Swept Wing Configuration
FLUID FLIGHT CONTROL SYSTEM ON TAP FOR SATURN
Flutter Tests of Some Simple Models at a Mach Number of 7.2 in Helium Flow
Free flight simulated on ground with the Apollo Saturn V space vehicle.
Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 317
Generalized Momentum Control of the Spin-Stabilized Magnetospheric Multiscale (MMS) Formation
Global Precipitation Measurement Mission Launch and Commissioning
Halo Orbit Mission Correction Maneuvers Using Optimal Control
Heat Pipes for Space Applications Part 1 - Axially Grooved Heat Pipes
High accuracy, high reliability infrared horizon sensors for earth, lunar, and planetary use.
High-power-level temperature controller for space flight applications
Investigation of an all-movable control surface at a mach number of 6.86 for possible flutter