STK AstrogatorSend comments on this topic.
AgEVABurnoutOptions Enumeration
See Also

Description

Burnout options for the Launch segment.

Members

MemberValueDescription
eVABurnoutOptionsFixedVelocity0Use 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.
eVABurnoutOptionsInertialVelocity1Use Inertial Velocity - the final state of the launch segment is solely and completely determined by the burnout position and velocity.
© 2025 Analytical Graphics, Inc. All Rights Reserved.