Path: LunarMissions/LunarMission
% Lunar polar mission planning Compute lunar transfer delta-Vs. The steps are: # Set the elements and date so that transfer orbit and lunar orbit match. # Compute the insertion delta-v # Circularize the lunar orbit # Do a Hohmann descent to the powered landing altitude See also: Constant, Date2JD, PlanetPosJPL, RV2El, MoonRot, Unit, RPRA2AE, RVOrbGen, VOrbit, DVHoh, RocketMass, DisplayLatexTable %
Orbit: OrbitCoord/RARP2A Orbit: OrbitCoord/RPRA2AE Orbit: OrbitManeuver/DVHoh Orbit: OrbitMechanics/RVOrbGen Orbit: Visualization/EarthMoon Propulsion: Rocket/RocketMass SC: BasicOrbit/Period SC: BasicOrbit/RV2El SC: BasicOrbit/VOrbit SC: Ephem/CEcl2Eq SC: Ephem/MoonRot SC: Ephem/PlanetPosJPL Common: Database/Constant Common: General/CreateLatexTable Common: General/DisplayLatexTable Common: Time/Date2JD Math: Linear/Mag Math: Linear/Unit
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