XB-28 Dragon - Definition and Overview

The XB-28 Dragon (North American model NA-63) was a plane proposed by the North American Aviation to fill a strong need in the United States Army Air Corps for a high-altitude medium bomber. It was never entered into production; only two aircraft were built.

Development

The order for a high-altitude medium bomber was put out on 1940 February 13; the XB-28 first flew on 1942 April 26. The XB-28 was based on North American Aviation’s highly successful B-25 Mitchell, but as it evolved it became a completely new design, much more reminiscent of the Martin B-26 Marauder. The overall configuration of the B-25 and XB-28 were fairly similar; the most important distinction was that the twin tail of the B-25 was changed to a single tail on the XB-28. It was among the first planes with a pressurised cabin.

The XB-28 proved an excellent design, with significantly better performance than the B-25, but it was never put into production. High-altitude bombing was hampered significantly by factors such as clouds and wind, which were frequent occurrences in the Pacific. At the same time, medium bombers were becoming much more able at lower altitudes. The models being used at these levels had been used successfully in combat for months and even years. The gains in aircraft performance made that came with high altitude flight were not significant enough to justify switching from low-altitude bombing.

Even though the Army Air Force rejected the XB-28 as a bomber, they ordered another prototype. Dubbed the XB-28A, it was meant to explore the possibility of use as a reconnaissance aircraft. This design never progressed passed the prototype stage, either.

Specifications (XB-28)

General Characteristics

• Crew: five
• Length: 56 ft 5 in (17.20 m)
• Wingspan: 72 ft 7 in (22.12 m)
• Height: 14 ft 0 in (4.27 m)
• Wing area: 676 ft² 62.8 m²
• Empty: 25,575 lb (11,600 kg)
• Loaded: 35,740 lb (16,210 kg)
• Maximum takeoff: 37,200 lb (16,874 kg)
• Powerplant: 2× Pratt & Whitney R-2800-27 turbosupercharged radial en-gines; 2,000 hp (1492 kW) each

Performance

• Maximum speed: 372 mph (446 km/h)
• Cruising speed: 255 mph (410 km/h)
• Range: 2,040 miles (3282 km)
• Service ceiling: 33,500 ft (10,213 m)
• Rate of climb: 1,111 ft/min (339 m/min)
• Wing loading: 52.87 lb/ft² (258.14 kg/m²)
• Power/Mass: 0.112 hp/lb (0.184 kW/kg)

Armament

• 6× .50-calibre machine gun (in remote-sighted turrets)
• 4,000 lb (1,818 kg) of bombs

References

• American Aircraft of World War II (http://www.daveswarbirds.com/usplanes/american.htm)
• Joe Baugher’s XB-28 site (http://www.csd.uwo.ca/~pettypi/elevon/baugher_us/b028-01.html)
• USAF Museum (http://www.wpafb.af.mil/museum/research/bombers/b3-27.htm)

Related content

Related development:

Comparable aircraft: B-26 Marauder - Martin XB-27

Designation sequence: B-25 - B-26 - XB-27 - XB-28 - B-29 - XB-30 - XB-31 -

See also:

• List of military aircraft of the United States
• List of bomber aircraft