Ram air turbine installation allowing low speed flight

A cargo aircraft, comprising:

• a fuselage defining a forward end, an aft end, and a continuous interior cargo bay that spans a majority of a length of the fuselage from the forward end to the aft end, the fuselage including:
• a forward portion containing a forward region of the continuous interior cargo bay, the forward portion defining a forward centerline along a longitudinal-lateral plane of the cargo aircraft,
• an aft portion containing an aft region of the continuous interior cargo bay, the aft portion defining an aft centerline extending above the longitudinal-lateral plane of the cargo aircraft, and
• a kinked portion forming a junction in the fuselage between the forward portion and the aft portion of the fuselage and between the forward and aft regions of the continuous interior cargo bay, the kinked portion containing a transition region of the continuous interior cargo bay and defining a bend angle between the forward centerline and the aft centerline;
• a first fixed wing extending from the fuselage in a first direction away from the fuselage;
• a second fixed wing extending from the fuselage in a second direction away from the fuselage, the second direction approximately symmetric about a longitudinal-vertical center plane of the cargo aircraft;
• and
• a ram air turbine coupled with the fuselage and configured to move between a retracted position where the ram air turbine is stowed inside fuselage and an extended position where the ram air turbine is disposed above a suction surface of the first fixed wing.