LaunchVehicleControlFixedApogeeAltitude
=======================================

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

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

   Class defining the option to set a Missile's flight parameters by specifying a fixed apogee altitude.

.. py:currentmodule:: LaunchVehicleControlFixedApogeeAltitude

Overview
--------

.. tab-set::

    .. tab-item:: Properties

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

            * - :py:attr:`~ansys.stk.core.stkobjects.LaunchVehicleControlFixedApogeeAltitude.apogee_altitude`
              - Fixed apogee altitude: the vehicle's maximum altitude. Uses Distance Dimension.



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

.. code-block:: python

    from ansys.stk.core.stkobjects import LaunchVehicleControlFixedApogeeAltitude


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

.. py:property:: apogee_altitude
    :canonical: ansys.stk.core.stkobjects.LaunchVehicleControlFixedApogeeAltitude.apogee_altitude
    :type: float

    Fixed apogee altitude: the vehicle's maximum altitude. Uses Distance Dimension.