Path: Orbit/OrbitManeuver

% Compute the total delta-V for the JIMO mission
   This mission assumes a low thrust
   The time is in seconds and is 4 months
   The vehicle low thrust spirals out of earth orbit then low thrust
   spirals to Callisto. It goes into orbit about Callisto and repeats
   with the other planets. 

   Since version 10.


AC: ACData/ACTConstants
Orbit: OrbitManeuver/DVHoh
Orbit: OrbitManeuver/LTSpiral
Orbit: OrbitManeuver/LowThrustEscape
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/CreateLatexTable
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

Back to the Orbit Module page