public void TestOozinozSkyocket()
{
double burnArea = .0030;
double burnDepth = .06;
double burnVolume = burnArea * burnDepth;
double fuelMass = burnVolume * FUEL_DENSITY;
double totalMass = fuelMass * 1.1;
double burnRate = .020;
PhysicalRocket pr = new PhysicalRocket(burnArea, burnRate, fuelMass, totalMass);
OozinozSkyrocket or = new OozinozSkyrocket(pr);
double tol = 0.01;
or.SetSimTime(0);
Assert.AreEqual(totalMass, or.GetMass(), tol, "initial mass");
Assert.AreEqual(SPECIFIC_IMPULSE * FUEL_DENSITY * burnArea * burnRate, or.GetThrust(), tol, "thrust");
double bt = burnDepth / burnRate;
or.SetSimTime(bt * 1.01);
Assert.AreEqual(totalMass - fuelMass, or.GetMass(), tol, "end mass");
Assert.AreEqual(0, or.GetThrust(), tol, "thrust");
}
public void TestOozinozSkyocket()
{
double burnArea = .0030;
double burnDepth = .06;
double burnVolume = burnArea * burnDepth;
double fuelMass = burnVolume * FUEL_DENSITY;
double totalMass = fuelMass * 1.1;
double burnRate = .020;
PhysicalRocket pr = new PhysicalRocket(burnArea, burnRate, fuelMass, totalMass);
OozinozSkyrocket or = new OozinozSkyrocket(pr);
double tol = 0.01;
or.SetSimTime(0);
Assertion.AssertEquals("masa pocz¹tkowa", totalMass, or.GetMass(), tol);
Assertion.AssertEquals("ci¹g", SPECIFIC_IMPULSE * FUEL_DENSITY * burnArea * burnRate, or.GetThrust(), tol);
double bt = burnDepth / burnRate;
or.SetSimTime(bt * 1.01);
Assertion.AssertEquals("masa koñcowa", totalMass - fuelMass, or.GetMass(), tol);
Assertion.AssertEquals("ci¹g", 0, or.GetThrust(), tol);
}