Convair

Consolidated Vultee XP-81

The Consolidated Vultee XP-81 was an experimental fighter‑interceptor developed by Convair in the early 1940s as the United States sought a high‑performance aircraft capable of countering emerging jet threats. Initiated in 1943, the XP‑81 combined a powerful Wright R-2600 radial engine with a Westinghouse J33 turbo‑jet, forming one of the first true mixed‑propulsion designs. Its sleek, low‑wing airframe featured a laminar‑flow wing, tricycle landing gear, and a pressurized cockpit that accommodated a single pilot with advanced instrumentation. Armament plans called for four 20 mm cannons and provisions for rockets or bombs, giving it a versatile attack profile. Although flight testing in 1945 demonstrated impressive climb rates and a top speed near 600 mph, development was curtailed by rapid advances in pure‑jet technology and the end of World War II. The XP‑81 never entered production, but its dual‑engine configuration informed later Convair projects such as the F‑102 Delta Dagger and contributed valuable data on engine integration, cooling, and aerodynamic stability. As a transitional prototype, the XP‑81 represents a pivotal step in the evolution from piston‑powered fighters to the jet age, highlighting the innovative engineering challenges of the era.

Classification

Production & History

First Flight
1945

Design & Classification

Manufacturer
Convair
Wikidata ID
Q1129337