Schubkraft(F) = Duchsatz(q) * Massenstrom(m)
Schubkraft(F) = Querschnitt(A)m² * Dichte(p)Kg/m³ * Massenstrom(m)²

Massenstrom(m)Kg/s = Dichte(p)Kg/m³ * Mittlere Strömungsgeschwindigkeit(c)m/s * Querschnitt(A)m²
Massenstrom(m)Kg/s = Dichte(p)Kg/m³ * Volumenstrom(V)m³/s

Volumenstrom(V)m³/s = Volumen(V)m³/0


Luftdichte bei 25°C = 1.1839 Kg/m³
Dt = 0.02m

F = A * p * m
F = A * p * p * V
F = A * p² * V
F = Dt * PI * 1.1839² * ( Dt * PI * 1.1839)
F = 0.02 * 3.14 * 1.1839² * (0.02 * 3.14 * 1.1839)
F = 0.088021686388 * 0.07434892
F = 0.00654431731952650096 ~ 0.006N





F = q * Ve + (Pe - Pa) * Ae

q = Propellant mass flow rate
Ve = Velocity of exhaust gases
Pe = Pressure at nozzle exit
Pa = Ambient pressure
Ae = Area of nozzle exit