#include <SpacecraftParam.hpp>
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double | cd () const |
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void | setCd (double cd) |
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double | cr () const |
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void | setCr (double cr) |
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double | dragArea () const |
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void | setDragArea (double dragArea) |
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double | srpArea () const |
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void | setSrpArea (double srpArea) |
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double | mass () const |
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double | dryMass () const |
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void | setDryMass (double dryMass) |
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double | fuelMass () const |
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void | setFuelMass (double fuelMass) |
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double | fuelDensity () const |
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void | setFuelDensity (double fuelDensity) |
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double | k1 () const |
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void | setK1 (double k1) |
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double | k2 () const |
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void | setK2 (double k2) |
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double | radPressureArea () const |
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void | setRadPressureArea (double radPressureArea) |
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double | radPressureCoeff () const |
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void | setRadPressureCoeff (double radPressureCoeff) |
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double | tankPressure () const |
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void | setTankPressure (double tankPressure) |
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double | tankTemperature () const |
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void | setTankTemperature (double tankTemperature) |
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double | cd_ {2.2} |
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double | cr_ {1} |
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double | dragArea_ {20} |
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double | srpArea_ {20} |
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double | dryMass_ {500} |
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double | fuelMass_ {500} |
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double | fuelDensity_ {1000} |
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double | k1_ {1} |
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double | k2_ {1} |
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double | radPressureArea_ {20} |
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double | radPressureCoeff_ {1} |
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double | tankPressure_ {5000} |
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double | tankTemperature_ {293.15} |
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