NASA NTRS · 19650026376
Conic solutions to the interplanetary transfer problem with constant or minimum injection energy
Abstract
Minimum and constant energy values for injection into launch window to achieve interplanetary spacecraft trajectory
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Bullock, L. E.. 1965-08-16. Conic solutions to the interplanetary transfer problem with constant or minimum injection energy. https://ntrs.nasa.gov/citations/19650026376
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