NASA NTRS · 19720018867
Improved guidance hardware study for the scout launch vehicle
Abstract
A market survey and evaluation of inertial guidance systems (inertial measurement units and digital computers) were made. Comparisons were made to determine the candidate systems for use in the Scout launch vehicle. Error analyses were made using typical Scout trajectories. A reaction control system was sized for the fourth stage. The guidance hardware to Scout vehicle interface was listed.
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Schappell, R. T., Salis, M. L., Mueller, R., Best, L. E., Bradt, A. J., Harrison, R., Burrell, J. H.. 1972-06-01. Improved guidance hardware study for the scout launch vehicle. https://ntrs.nasa.gov/citations/19720018867
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