Vibrator (Cornell-Dubilier 5622-S) Environmental Performance Evaluation
Aerodynamic Analysis of a Low Density Hypersonic Shock-Wind Tunnel
A Reliable Galvanometer Movement for Use in Space Applications
Jet Propulsion Laboratory High-Intensity Acoustic Test System
Measurement of Flow Speed and Flow Direction by Aerodynamic Probes and Vanes
Stability and Control Flight Testing - Some of the Test Instrumentation Requirements
Development of an Isotropic Radiation Simulator
Performance Analysis of a Low-Range Vibrating- Contact Pressure Transducer
Development of a Non-Magnetic Flight Type Mass Spectrometer Final Report
Feasibility Studies of a Short Duration High Reynolds Number Tube Wind Tunnel
Wind Tunnel Tests in the Field of Industrial Aerodynamics
Development, Testing and Measuring of a Circuit Hot Air Wind Tunnel
Performance Characteristics of Liquid-Vapor Sensors Operating in a Reduced Gravity Environment
Infrared Testing of Electronic Components
Development and Testing of the Lunar Gravity and Earth Orbital Simulator (Parallelogram)
Low Gravity Fluid Mechanics Drop Tower Facility
Development of a 3-Component Strain-Gauge for Use on the Whirling ARM