IsothermalCubeSatDemo:

Path: CubeSat/Thermal

% Isothermal satellite demo
 The entire CubeSat is assumed to be at the same temperature. This is a
 very useful first approximation of the spacecraft temperatures on orbit.
 The oscillations in the temperatute reflect the eclipses. This demo
 includes solar flux, internal power, and planetary fluxes are optional.

 Model a 3U satellite with different materials comprising the faces. Each
 area is 1U for a total of 14 surfaces. The surfaces are either solar
 cell, gold foil, or radiator.

 See also RHSIsothermalCubeSat, CubeSatEnvironment
%
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   Copyright (c) 2009-2010,2014 Princeton Satellite Systems, Inc.
   All rights reserved.
  2025.1 Update to use CubeSatEnvironment and allow for planetary fluxes
  as well as solar flux.
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Children:

AerospaceUtils: Coord/QLVLH
CubeSat: Simulation/CubeSatEnvironment
CubeSat: Thermal/RHSIsothermalCubeSat
Orbit: OrbitMechanics/Period
Orbit: OrbitSim/RVFromKepler
Common: Graphics/AddFillToPlots
Common: Graphics/Plot2D
Common: Quaternion/QForm
Common: Time/FindSolsticeOrEquinox
Math: Integration/RK4

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