AGI STK Astrogator 11 Send comments on this topic.
AgEVABurnoutOptions Enumeration
See Also 

Description

Burnout options for the Launch segment.

Members

Member Value Description
eVABurnoutOptionsFixedVelocity 0 Use Fixed Velocity - the inclination of the final state of the launch segment is determined by the arc between the launch and insertion positions, and the horizontal flight path angle is set to zero.
eVABurnoutOptionsInertialVelocity 1 Use Inertial Velocity - the final state of the launch segment is solely and completely determined by the burnout position and velocity.
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STK Programming Interface 11.0.1