Comparison of the Lateral Motion Calculated for Tailless and Conventional Airplanes
Design and Test of Low-Profile Composite Aerospace Tank Dome
Blade Motion Correlation for the Full-Scale UH-60A Airloads Rotor
Influence of Imperfections and Edge Restraint on the Buckling of Axially Compressed Cylinders
Effect of Predicted Vehicle Displacement on Ground Crew Task Performance and Hardware Design
Effect of Yaw Angle on Steering Forces for the Lunar Roving Vehicle Wheel
Single-Point Attachment Wind Damper for Launch Vehicle On-Pad Motion
Orion MPCV Service Module Avionics Ring Pallet Testing, Correlation, and Analysis
Hydrodynamic Journal Bearing Program Quarterly Progress Report, 29 Apr. - 29 Jul. 1966
Thrust Stand for Electric Propulsion Performance Evaluation
Measurements and Analysis of Solid Propellant Rocket Vibrations Obtained During a Captive Flight
A Study of Stiffness Matrices for the Analysis of Flat Plates
Active and Adaptive Control for Payload Launch Vibration Isolation
Development of a Horizontal Impact Sled Facility and Subsequent Crashworthiness Experiments
Investigating the Deformation and Failure Mechanisms in Bi-Material Systems Under Tension
Missile Launcher Integral Shock Isolation and Running Gear System
Flying Quality Analysis of a JAS 39 Gripen Ministick Controller in an F/A-18 Aircraft
The Influence of Surface Curvature on Two-Dimensional Laminar Boundary Layers
Characterization of Space Shuttle Ascent Debris Aerodynamics Using CFD Methods
Development and Evaluation of Steering Assembly Countermeasures
Space Radiation Equivalence for Effects on Transistors Final Report, 15 May 1965 - 15 Nov. 1966
Flight Characteristics Test of the UH-60A with Tail Boom Mounted Strake
Solar Array Thermal Snap and the Characteristics of Its Effect on UARS
Momentum Flux Measurements from Under Expanded Orifices: Applications for Micropropulsion Systems
Flight Test of an 8000 PSI Lightweight Hydraulic System (LHS)
Effect of Steady Aerodynamic Loading on the Flutter Stability of Turbomachinery Blading
High Accuracy Attitude Control of a Spacecraft Using Feedback Linearization
Missile Dynamics Equations for Guidance and Control Modeling and Analysis
Installation and Test of a Hydrostatic Drive Transmission in a Government Furnished M-113 Vehicle
Second Joint NASA/FAA/DoD Conference on Aging Aircraft, Part 2