NASA NTRS · 19790017926
Transfer trajectory design for a shuttle launched geosynchronous payload
Abstract
The firing of a fixed impulse spin stabilized upper stage following shuttle deployment of a geosynchronous payload was examined in detail. Design of the transfer trajectory was discussed in terms of finding both a nominal and possible dispersion case that can be handled operationally within the allotted trim fuel budget.
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Defazio, R. L.. 1979-04-01. Transfer trajectory design for a shuttle launched geosynchronous payload. https://ntrs.nasa.gov/citations/19790017926
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