XB-28 Dragon
The
North American XB-28 Dragon (
North American 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 never entered into full production and only two aircraft were built.
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. Designated
XB-28A, it was meant to explore the possibility of use as a reconnaissance aircraft. This design never progressed passed the prototype stage either.
{{aircraft specifications
plane or copter?=plane | >crew=five | length main=56 ft 5 in | length alt=17.20 m | span main=72 ft 7 in | span alt=22.12 m | height main=14 ft 0 in | height alt=4.27 m | area main=676 ft² | area alt=62.8 m² | empty weight main=25,575 lb | empty weight alt=11,600 kg | loaded weight main=35,740 lb | loaded weight alt=16,210 kg | max takeoff weight main=37,200 lb | engine (prop)=Pratt & Whitney R-2800-27 | type of prop=turbosupercharged radial engines | number of props=2 | power main=2,000 hp | max speed main=372 mph | max speed alt=446 km/h | max speed more=at 25,000 ft (7,600 m) | cruise speed main=255 mph | cruise speed alt=410 km/h | range main=2,040 mi | range alt=3,280 km | ceiling main=33,500 ft | ceiling alt=10,213 m | climb rate main=1,111 ft/min | climb rate alt=6 m/s | loading main=52.87 lb/ft² | loading alt=258.14 kg/m² | power/mass main=0.112 hp/lb | guns=6× .50 in (12.7 mm) machine guns in remote-sighted turrets | bombs=4,000 lb (1,800 kg)*Joe Baugher's Encyclopedia of American Aircraft *USAF Museum{{aircontent|related= * B-25 Mitchell|similar aircraft= * B-26 Marauder * Martin XB-27|sequence= * B-25 - B-26 - XB-27 - XB-28 - B-29 - XB-30 - XB-31|lists= * List of military aircraft of the United States * List of bomber aircraft|see also=
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