LunarMissionDesign:

%  Lunar mission planning
 Compute transfer delta-Vs and simulate a lunar landing starting from 
 low Earth orbit. The entire spacecraft lands, there is no portion left in
 lunar orbit. 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
 # Do a powered landing using BilinearTangent
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  See also RARP2A, RPRA2AE, DVHoh, RVOrbGen, EarthMoon, TrajectoryPlot, 
  RocketMass, Period, RV2El, VOrbit, CEcl2Eq, PlanetPosJPL, 
  BilinearTangentLaw, Constant, CreateHTMLTable, DisplayLatexTable, NewFig, 
  TimeLabl, XLabelS, Date2JD, RK4, Mag
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%
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   Copyright (c) 2014 Princeton Satellite Systems
   All Rights Reserved.
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Children:

Common: Database/Constant
Common: General/CreateHTMLTable
Common: Graphics/DisplayLatexTable
Common: Graphics/NewFig
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Time/Date2JD
Math: Integration/RK4
Math: Linear/Mag
Orbit: OrbitCoord/RARP2A
Orbit: OrbitCoord/RPRA2AE
Orbit: OrbitManeuver/DVHoh
Orbit: OrbitMechanics/RVOrbGen
Orbit: Visualization/EarthMoon
Orbit: Visualization/TrajectoryPlot
Propulsion: Rocket/RocketMass
SC: BasicOrbit/Period
SC: BasicOrbit/RV2El
SC: BasicOrbit/VOrbit
SC: Ephem/CEcl2Eq
SC: Ephem/PlanetPosJPL
SCPro: Landers/BilinearTangentLaw