NASA NTRS · 19670004915
Dynamics and control research applicable to Apollo extension systems
Abstract
Disturbance envelope and experiment requirements for Apollo missions used to determine optimum control-moment gyro-jet system
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Keckler, C. R., Kurzhals, P. R., Piland, W. M.. 1966-12-01. Dynamics and control research applicable to Apollo extension systems. https://ntrs.nasa.gov/citations/19670004915
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