Path: Propulsion/Rocket
% Finds the minimum exhaust velocity based on the structural ratio. Type MinimumExhaustVelocity for a demo. -------------------------------------------------------------------------- Form: uE = MinimumExhaustVelocity( sR, dV ) -------------------------------------------------------------------------- ------ Inputs ------ sR (1,:) Structural ratio dV (1,:) Delta V ------- Outputs ------- uE (1,:) Minimum exhaust velocity --------------------------------------------------------------------------
Common: Graphics/Plot2D
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