LaunchVehicleControlFixedDeltaVMinimumEccentricity
==================================================

.. py:class:: ansys.stk.core.stkobjects.LaunchVehicleControlFixedDeltaVMinimumEccentricity

   Bases: :py:class:`~ansys.stk.core.stkobjects.IVehicleLaunchControl`

   Class defining the option to set a Missile's flight parameters by specifying a fixed delta V with minimum eccentricity.

.. py:currentmodule:: LaunchVehicleControlFixedDeltaVMinimumEccentricity

Overview
--------

.. tab-set::

    .. tab-item:: Properties

        .. list-table::
            :header-rows: 0
            :widths: auto

            * - :py:attr:`~ansys.stk.core.stkobjects.LaunchVehicleControlFixedDeltaVMinimumEccentricity.delta_v_min`
              - Fixed Delta V minimum eccentricity. Uses Rate Dimension.



Import detail
-------------

.. code-block:: python

    from ansys.stk.core.stkobjects import LaunchVehicleControlFixedDeltaVMinimumEccentricity


Property detail
---------------

.. py:property:: delta_v_min
    :canonical: ansys.stk.core.stkobjects.LaunchVehicleControlFixedDeltaVMinimumEccentricity.delta_v_min
    :type: float

    Fixed Delta V minimum eccentricity. Uses Rate Dimension.