More/less efficient ascents are likely depending on ascent profile, TWR and aerodynamic effects. Total values do not include maximum plane change Delta V. All values are measured as vacuum Delta V in m/s. Low orbits are 10 km above the atmosphere or terrain obstacles. Obtain the planetary phase angle, ejection angle and ejection velocity values according to your. For optimal efficiency, make this orbit at a 90° heading. Map design by /u/swashlebucky, based on Kowgan’s map for 1.0.4, design inspired by Kowgan and WAC, atmospheric numbers by Kowgan, Vacuum numbers by /u/CuriousMetaphor, additional vacuum numbers by Armisael, Relay Antenna calculations from the Wiki, and original subway concept by /u/Jell圜ubes Using these values for interplanetary flight is no more complicated than obtaining them: Place your ship in a circular, 0° inclination parking orbit around your planet/moon of origin. If you want to download the map, find it here Official Wiki (Relay Antenna calculations) Kowgan (Design, original in-atmosphere numbers) CuriousMetaphor (Original out-of-atmosphere numbers)Īrmisael (Additional out-of-atmosphere numbers)
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