diff --git a/functions/miscellaneous/getXCP.m b/functions/miscellaneous/getXCP.m
index a89d3548ee56634b03680af9cb14222acda00a78..81ed070649bd59df61581c914dcf191c9ea1643c 100644
--- a/functions/miscellaneous/getXCP.m
+++ b/functions/miscellaneous/getXCP.m
@@ -99,7 +99,11 @@ else
     XCPvect(5) = Mrot(1)/Frot(2);   % Longitudinal
     XCPvect(6) = -Mrot(2)/Frot(1);  % Lateral
 end
-
+%%% OPEN ROCKET
+% if vars.checkOpenRocket
+%     angle = getAlphaPhi(input.fltcon.ALPHA(iAlpha)*pi/180, input.fltcon.BETA(iBeta)*pi/180);
+%     XCPvect(7) = aerodynamics(input, angle, vars.modHaack);
+% end
 %% SAVE COEFFICIENTS
 stabilityCoeffs = [Cma CNA Cm CN Cnb CYB Cn CY Cl CA Frot(1) Frot(2) Mrot(1) Mrot(2)]';