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The Effect of Length on the Aerodynamic Characteristics of Bodies of Revolution in Supersonic Flight
Evaluation of the Kellett Gyratory Stabilizer Installed on the H-21 Helicopter
Free-Spinning Characteristics of a 1/30-Scale Model of the Grumman WF-2 Airplane
Free-Spinning-Tunnel Investigation of a 1/30 Scale Model of a Twin-Jet-Swept-Wing Fighter Airplane
Spin Testing ... United States Navy High Performance Airplanes
SIMULATOR STUDIES OF SIMPLE ATTITUDE CONTROL FOR SPIN-STABILIZED VEHICLES
Effect of Dynamic Imbalance on the Motion of a Spinning Vehicle in Free Flight
MINIGUIDE - A SIMPLIFIED ATTITUDE CONTROL FOR SPINSTABILIZED VEHICLES
Satellite attitude determination - Digital sensing and on-board processing
Spin Investigation Of A 1/20-Scale Model Of An Unswept-Wing, Twin-Engine, Observation Airplane
Design and evaluation study of deployable solar array for spinning satellites Final report
Design and Evaluation Study of Deployable Solar Array for Spinning Satellites Final Report
Miniguide - a simplified attitude control for spin-stabilized vehicles
Nasa to launch sert i spacecraft news release no. 64-167
Symposium on Parachute Technology and Evaluation, Proceedings. Volume II
Attitude Determination of Spin Stabilized Spacecraft Using a Digital Aspect Sensor
Pendulum-Type Nutation Damper Used in the NASA Atmospheric Structure Satellite, S-6
Attitude determination of spin stabilized spacecraft using a digital aspect sensor
Some design considerations for spin-stabilized satellites with rigid expandable structures
Scanning celestial attitude determination system /SCADS/.
Pendulum-type nutation damper used in the nasa atmospheric structure satellite, s-6
Attitude stabilization using a contactor control system with a linear switching criterion.
A passive pendulum wobble damping system for the nasa 21 man rotating space station.
Eldo Apogee Stage. Eldo Future Programmes. Project No. 1, Study No. 1.5 - U.K. study
Aerodynamic Deployable Decelerator Performance - Evaluation Program
A viscous ring damper for a freely precessing satellite.
Spinning satellite attitude control via the Earth's magnetic field.
Motion of a spinning satellite during the deployment of asymmetrical appendages.
Motion of a spinning satellite during the deployment of n asymmetrical appendages.
Attitude Perturbations and Magnetic Control of a Spin-Stabilized Satellite, Part II