Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
Tests of a 45 deg Sweptback-Wing Model in the Langley Gust Tunnel
Design and Evaluation Study of Deployable Solar Array for Spinning Satellites Final Report
Development of Three Types of Flat Flexible Conductors Final Report, Aug. 1963 - Feb. 1964
The Aeroelastic Characteristics of the Saturn-Ib Sa-201 Launch Vehicle
Control Techniques for Large Launch Vehicles Final Report, Jul. 1964 - Sep. 1965
Evaluation Polyurethane Elastomeric Compound CS-3547, Type III
Preliminary Experiments on the Influence of Flexible Walls on Boundary Layer Turbulence
Development of a Prototype Plastic Space Erectable Satellite Quarterly Report, Sep. - Nov. 1965
Polyurethane Elastomeric Compound Cps 796-80, Type III Qualification Test Report