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Preliminary Results from Propellant Mass Gauging with Electrical Capacitance Tomography
Characteristics of Separated Flow Regions Within Altitude Compensating Nozzles Final Report
Study of active vibration isolation systems for severe ground transportation environments
Advanced feed system component interaction analysis Quarterly status letter, 30 Jun. - 30 Sep. 1969
Progress of CFM Model Development and Validation at NASA Glenn Research Center
Reducing Landing Site Contamination Using 3-D Trajectory Optimization for Surface Hoppers
A Shock Tube Driver with a 'Cyclone' Separator
Canadian Space Launch: Exploiting Northern Latitudes for Efficient Space Launch
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Dynamic vibration absorbers : theory and technical applications
Cryogenic Propellant Tank Self-Pressurization and Active Pressure Control
Propellant Mass Gauging in Microgravity with Electrical Capacitance Tomography
Liquid propellant losses during space flight final report, sep. 1, 1960 - sep. 30, 1963
Four Preliminary Designs for Hydrodynamic Prototypes of 36 Foot Hydrofoil Landing Craft
Propellant Mass Gauging in Microgravity with Electrical Capacitance Tomography
Suppression of aerodynamically induced cavity pressure oscillations
The Long-Term Motion of Artificial Planetary Satellites
Hypervelocity impact effects on liquid hydrogen tanks Final report, 1 Jul. 1964 - 30 Nov. 1965
Capacitance-Torsion Balance for Measuring Small Stresses and Strains
Stake Driving Tools. A Preliminary Survey
Biphase turbine for reverse osmosis desalination
Summary of Information Relating to Gust Loads on Airplanes
Cryogenic Fluid Technologies for Long Duration In-Space Operations
Momment on 'Review of Theoretical Investigations on Effect of Heat Transfer on Laminar Separation
Development of the Two Phase Flow Separator Experiment for a Reduced Gravity Aircraft Flight
On-Orbit ACDS Performance of the Landsat 7 Spacecraft
Using New Technologies to Characterize and Reduce Whole Body Vibration Exposures
Flying Infrared Telescope Final Report, 1 Apr. 1967 - 31 May 1971