Path: Missions/LunarMission
% Returns thrust and exhaust velocity for a rocket engine.
--------------------------------------------------------------------------
Form:
[thrust, uE] = FThrustLander( massFuel, d )
--------------------------------------------------------------------------
------
Inputs
------
massFuel (1,1) Mass of fuel (kg)
d (.) Data structure
.thrust (1,1) Thrust magnitude (N)
.uE (1,1) Exhaust velocity (m/s)
.uThrust (3,1) Thrust unit vector
-------
Outputs
-------
thrust (3,1) Thrust vector (N)
uE (1,1) Exhaust velocity (m/s)
--------------------------------------------------------------------------
Back to the Missions Module page