NASA NTRS · 19760064257
New thruster configurations for spacecraft attitude control systems
Abstract
Design characteristics of thruster configurations for spacecraft attitude control systems investigated. A standard six engine approach is developed and used as the basis for comparison of different thruster configurations. These methods include cases of both skewed and non-skewed configurations. Simulation results are used as a basis for comparison, critical thruster design factors being given based on an analysis of the data.
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Colburn, B. K., Chakravarthi, K. R., Drinkard, D. M., Boland, J. S., III. 1976-01-01. New thruster configurations for spacecraft attitude control systems. https://ntrs.nasa.gov/citations/19760064257
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