Tag Archives: Martin XB-10

16 February 1932

Martin XB-907 in flight. (U.S. Air Force 060511-F-1234S-002)

16 February 1932: First flight, Glenn L. Martin Co. Model 123, designated XB-907 by the U. S. Army Air Corps. It was a streamlined all-metal mid-wing monoplane with retractable landing gear. It had an internal bomb bay. The airplane was flown by a single pilot and had two gunners, all in open cockpits.

The Model 123 was a private venture, designed and built at a cost of more than $200,000.

On 26 February 1932, the Model 123 was flown from the Martin plant in Middle River, Maryland, to the Aberdeen Proving Grounds by a U.S. Army Air Corps crew.

The XB-907 was powered by two air-cooled, supercharged 1,823.129-cubic-inch-displacement (29.875 liter) Wright Cyclone SR-1820-E nine-cylinder radial engines, rated at 600 horsepower, each. The engines were covered by Townend rings to reduce drag and improve cooling.

Martin XB-907

The prototype was tested at Wright Field. The airplane reached a maximum speed of 197 miles per hour (317 kilometers per hour) at 6,000 feet (1,829 meters). Recommendations for modifications were made, and Martin upgraded the prototype to the XB-907A configuration (Martin Model 139), which was then designated XB-10 by the Air Corps, with the serial number 33-139.

Martin XB-907A, right profile. (U.S. Air Force)

Martin increased the XB-907A’s wingspan from 62 feet, 2 inches (18.948 meters) to 70 feet, 7 inches (21.514 meters). The engines were upgraded to Wright R-1820-19s, rated at 675 horsepower. Full NACA cowlings were installed.

The Army then ordered 48 production airplanes.

The XB-907 would be developed into the Martin B-10 bomber.

U.S. Army Air Corps Martin B-10B of the 28th Bombardment Squadron, Philippine Islands 28 November 1939. (U.S. Air force)

© 2019, Bryan R. Swopes