The following list outlines the Missile Datcom outputs available through the AIM interface.

Forces and moments:

• CNtot = Normal Force Coefficient (body axis).
• CAtot = Axial Force Coefficient (body axis).
• CYtot = Side Force Coefficient (body axis).
• Cmtot = Pitching Moment Coefficient (body axis).
• Cntot = Yawing Moment Coefficient (body axis).
• Cltot = Rolling Moment Coefficient (body axis).
• CLtot = Lift Coefficient (wind axis).
• CDtot = Drag Coefficient (wind axis).
• Xcp = Center of Pressure in calibers from the moment reference center.

Derivatives - Alpha:

• CNa = Normal force coefficient derivative with angle of attack.
• Cma = Pitching moment coefficient derivative with angle of attack.

Derivatives - Beta:

• CYb = Side force coefficient derivative with sideslip angle.
• Cnb = Yawing moment coefficient derivative with sideslip angle (body axis).
• Clb = Rolling moment coefficient derivative with sideslip angle (body axis).

Echo inputs for case specific information:

• Alpha = Angle of attack from output file.
• Mach = Mach number from output file.
• Altitude = Altitude from output file.