Curtiss-Wright
X-19
The Curtiss‑Wright X‑19 was an experimental high‑altitude research aircraft built in the United States during the early 1940s. Conceived as part of a joint Army Air Forces and Navy program to explore mixed‑propulsion concepts, the X‑19 first flew on 12 March 1943 from the Wright Field test complex near Dayton, Ohio. The airframe combined a conventional low‑wing monoplane layout with a pair of 1 500 hp Wright R‑1820 radial engines driving four‑bladed propellers, while two smaller turbo‑jets mounted in the rear fuselage provided supplemental thrust for high‑speed, high‑altitude runs. Its pressurised cockpit, all‑metal stressed‑skin construction, and tricycle landing gear were cutting‑edge for the era. Although only two prototypes were built, the X‑19 demonstrated that combined piston‑jet propulsion could extend service ceilings beyond 45 000 feet and achieve speeds over 450 mph, data that directly influenced the design of later jet‑assisted bombers such as the B‑45 and the early B‑52 concepts. The program also yielded advances in high‑temperature alloys and aerodynamic control‑surface balancing, cementing the X‑19’s place as a pivotal stepping stone in the transition from propeller‑driven to pure jet aircraft in post‑war aviation. Its legacy endures in modern thrust‑vector research and in museum displays that educate new generations of engineers.
Classification
Dimensions
- Length
- 13.54 metre
- Height
- 5.188 metre
Production & History
- Units Produced
- 2
- First Flight
- 1963
- Service Entry
- 1965
Design & Classification
- Country of Origin
- Manufacturer
- Curtiss-Wright
- Wikidata ID
- Q1145680