Path: Missions/Comsat
% Computes the thrust and fuel consumed for thrusters. The units in this model will depend on the units in the database. p must correspond to the database units. Since version 1. -------------------------------------------------------------------------- Form: [thrust, dF, impulse, iSP] = REA( id, p, dT, database ) -------------------------------------------------------------------------- ------ Inputs ------ id (:) Thruster ids p (:) Pressure dT (:) Pulsewidth (sec) database (1,:) Database name ------- Outputs ------- thrust (:) Thrust dF (:) Fuel consumed impulse (:) Total impulse per thruster iSp (:) Specific impulse --------------------------------------------------------------------------
Math: Linear/SumC
Back to the Missions Module page