An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0
Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle
The Secular Outlook
Heat-transfer and Pressure Distributions at Mach Numbers of 6.0 and 9.6 Over Two Reentry Configurations for the Five-stage Scout Vehicle
Effect of Controlled Surface Roughness on Boundary-layer Transition and Heat Transfer at Mach Numbers of 4.8 and 6.0
Definition of Lateral-range and Lift-drag-ratio Requirements for Return to Both Optimum and Nonoptiumum Recovery Sites
Definition of Lateral-range and Lift-drag-ratio Requirements for Return to Both Optimum and Nonoptimum Recovery Sites
An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0
The Orbital Recovery Problem
Effects of Cloud Cover on Selection of Recovery Sites for Future Earth Orbital Missions
Orbital Recovery Program
Application of Analysis Technique to Selection of Recovery Sites for Return from Low Circular Orbits
Comparative Analyses of Space-to-space Central Power Stations
Roughness Effects on Boundary-layer Transition for Blunt-leading-edge Plates at Mach 6
Comparative Analyses of Space-to-space Central Power Stations
The Orbital Recovery Problem
An Investigation of Heat Transfer Within Regions of Separated Flow at a Mach Number of 6.0
An Analysis Technique for Rapid Determination of Return Opportunities and Lateral-range Requirements for Recall to Recovery Networks
The Orbital Recovery Problem