Two new methods have been developed to approximate pitch damping as a function of both angle of attack and Mach number. The newmethods can be used over theMach number (0–20) and angle-of-attack range (0–90 deg) of the Aeroprediction Code. The first method is based on the static nonlinear loads on the body and lifting surfaces that are available in the AeropredictionCode. The secondmethod is based on the improved linear value of pitch damping that was recently developed for the Aeroprediction Code. Recent improvements to the linear value include accuracy improvements for configurationswith long boattails and double counting of the body length beneath a lifting surface. Amethodwas derived to relate the zero angle-of-attack value of the pitch damping to a nonlinear value at an angle of attack. Comparison of the two newmethods to experimental data shows that both methods give results which follow the trends of experimental data, but neither method is superior for all cases at all angles of attack. As a result, results for both methods will be computed and available to the user of the Aeroprediction Code. The new methods will be a part of the 2009 version of the Aeroprediction Code, the AP09.