Rocket.hpp File Reference

#include <janus/janus.hpp>

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Namespaces
namespace	vulcan
namespace	vulcan::propulsion
	Propulsion utilities for rocket, air-breathing, and electric systems.
namespace	vulcan::propulsion::rocket

Functions
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::thrust_from_mdot (const Scalar &mdot, const Scalar &Ve)
	Calculates thrust from mass flow rate and effective exhaust velocity.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::exhaust_velocity (const Scalar &Isp, double g0=9.80665)
	Calculates effective exhaust velocity from specific impulse.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::specific_impulse (const Scalar &thrust, const Scalar &mdot, double g0=9.80665)
	Calculates specific impulse from thrust, mass flow rate, and gravity.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::delta_v (const Scalar &Ve, const Scalar &m0, const Scalar &mf)
	Calculates Delta-V using the Tsiolkovsky rocket equation.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::propellant_mass (const Scalar &delta_v, const Scalar &m0, const Scalar &Ve)
	Calculates required propellant mass for a given Delta-V.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::mass_flow_rate (const Scalar &thrust, const Scalar &Ve)
	Calculates mass flow rate from thrust and exhaust velocity.
template<typename Scalar>
Scalar	vulcan::propulsion::rocket::burn_time (const Scalar &propellant_mass, const Scalar &mdot)
	Calculates burn time for a given propellant mass and flow rate.