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clear;
clc;

RA = 0.1;
RB = 0.1;

Power = 50;

RO = (28^2)/Power;

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%Heat Output Data




function [heat,water] = heatOutput(temperature)
  radiated = [4.351581809194265	162.4752545248869
5.004325259515571	157.88909313725492
7.3232822540781015	140.690987933635
8.30239742956006	134.54880750377075

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clear;
clc;

diameter = 32/12/3.28;
length = 20/12/3.28;
P = 1.0*6894.76;

mass1 = 60000/2.204;
mass2 = 30000/2.204;

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#!/usr/bin/env python3
#***************************************************************************
#  This file is part of Project Apollo - NASSP
#
#  Copyright 2023 Matthew Hume
#
#  Scenerio Update Utility
#
#  Project Apollo is free software; you can redistribute it and/or modify
#  it under the terms of the GNU General Public License as published by

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#Flow rate
clear;
clc;

size = 0.00500;
dt = .005;
Volume1 = 120;
Volume2 = 240;

mass = 300;

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%Tank Heater
clear;
clc;

nominal_heat = 200; %Watts
ramp_rate = 10.0;


Dt = .1;
heat = 0;

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clear;
clc;


T = linspace(0,500,2000);
V1 = [];
V2 = [];
V3 = [];

R = 8.31446261815324E-2; 	#L.bar.K^-1.mol^-1

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clear;
clc;

#O2 and H2 density
O2Tcrit = 154.7;
H2Tcrit = 33.2;
N2crit = 126.2;
temp1 = linspace(0,O2Tcrit,75);
temp2 = linspace(O2Tcrit,500,100);
temp3 = linspace(0,H2Tcrit,15);

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function [V] = BatVoltage(ChargeLevel,MaxChargeVoltage)
  ## ChargeLevel = 0.0 -- 1.0
  ## MaxChargeVoltage, voltage when ChargeLevel == 1.0
  V = (1.007921192669853 - 0.009537198357788667./(ChargeLevel+0.09727407714017093).^2).*MaxChargeVoltage;
end

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#include <iostream>
#include <thread>
#include <vector>
#include <mutex>
#include <functional>
#include <cmath>

//simple test function to give the CPU something  to do
void JobFunction(double dt) {
	double dtTemp = 0;