Conformal multi-function air-data probes

An air data probe for use in an aircraft body that defines an aerodynamic outer surface comprising:

• an air-data probe including:
• an additively manufactured inner member including integrally formed, monolithic structures including:
• a mandrel bulkhead defining a plurality of pneumatic chambers therein in fluid communication with an outer surface of the mandrel bulkhead through respective pressure ports;
• a plurality of pneumatic tubes extending aft of the mandrel bulkhead along a probe axis, each in fluid communication with a respective one of the plurality of pneumatic chambers;
• and
• an outer cover tip engaged about the mandrel bulkhead with a plurality of bores therethrough for fluid communication of outside air pressure into the plurality of pneumatic tubes through the outer cover tip, wherein the outer cover tip includes a forward surface and an aft surface aft of the forward surface along the probe axis, wherein the forward surface is flush, conformal, and continuous with the aerodynamic outer surface, and wherein the aft surface is configured to extend inside the aerodynamic outer surface,
• wherein the aerodynamic outer surface and the outer cover tip are not integrally formed, monolithic structures with one another,
• wherein the aerodynamic outer surface and the additively manufactured inner member are not integrally formed, monolithic structures with one another, and
• wherein the outer cover tip and the additively manufactured inner member are not integrally formed, monolithic structures with one another.