Path: Missions/Pluto
% Pluto mission delta-Vs using DFD, Lambert solutions Use Lambert to calculate the delta-V to Pluto over a range of transit times, from 2 to 10 years. Estimate the total mission mass using specific power to scale the spacecraft, plus allowing for a given tank fraction, thrust efficiency, and a payload of 1000 kg. See also Constant, SaveStructure, Plot2D, Plot3D, Date2JD, RK4, Mag, LambertTOF, VEscape, RocketMass, FOrbCart, RV2El, PlanetPosition
AC: ACData/ACTConstants Orbit: OrbitMechanics/LambertTOF Orbit: OrbitMechanics/VEscape Propulsion: Rocket/RocketMass SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/FOrbCart SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: Ephem/PlanetPosition SC: Ephem/Planets SC: Ephem/SolarSys SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/IsVersionAfter Common: General/MatToCell Common: General/SaveStructure Common: General/StringToTokens Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TextS Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Materials/AtomicMass Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2T Math: Integration/RK4 Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit FusionEngine: PlasmaPhysics/FusionReaction FusionEngine: PlasmaPhysics/PlasmaConstant FusionEngine: PlasmaPhysics/ReactionString FusionEngine: Reactor/He3MassFromPower
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