AltitudeThrust.hpp

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#pragma once
 
#include <janus/janus.hpp>
 
namespace vulcan::propulsion {

template <typename Scalar>
Scalar altitude_thrust(const Scalar &F_vac, const Scalar &P_atm, double P_exit,
                       double A_exit) {
    // Suppress unused parameter warning for P_exit if needed,
    // or we could use it if we were given F_mom instead of F_vac.
    (void)P_exit;
    return F_vac - P_atm * A_exit;
}

template <typename Scalar>
Scalar thrust_coefficient(const Scalar &thrust, const Scalar &P_chamber,
                          double A_throat) {
    return thrust / (P_chamber * A_throat);
}
 
} // namespace vulcan::propulsion