Workshop on Thrust Augmenting Ejectors
The state of the art of ejector technology is assessed and the desired direction of future studies in all aspects of ejector thrust augmenting systems is deliniated.
Engineering topics
Publications and source records attributed to Lopez, A. E..
The state of the art of ejector technology is assessed and the desired direction of future studies in all aspects of ejector thrust augmenting systems is deliniated.
Display system effectiveness for manual guidance of large launch vehicles using X-15 and flight simulators
Pilot/vehicle dynamics from flight test records, discussing close-loop attitude control tasks
Remote control device operated by movement of finger tips for manual control of spacecraft attitude
Attitude stabilization of manned spacecraft by twin gyros and pulse-modulated reaction jets
Twin gyroscopic control system for three orthogonal axes of space vehicle attitude control
Automatic closed loop and pilot operated twin-gyro systems are discussed as attitude stabilizers for large space vehicles
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