NASA NTRS · 19660022768
An approximation method for determination of propulsion requirements associated with low thrust coplanar orbital transfer in a central force field under negligible external perturbations
Abstract
Approximation method for orbital transfer propulsion system requirements in central force field
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Duck, K. I.. 1963-01-01. An approximation method for determination of propulsion requirements associated with low thrust coplanar orbital transfer in a central force field under negligible external perturbations. https://ntrs.nasa.gov/citations/19660022768
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