XB-51
Specifications | ||
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Manufacturer (Airframe): | The Glenn L. Martin CO., Baltimore Md. | |
Manufacturer (Engines): | The General Electric CO.; Schenectady, N.Y. | |
Nomenclature: | Light Bomber | |
Span: | 53 feet, 1 inch | |
Length: | 85 feet, 1 inch | |
Wing Area: | 548 sq. ft. | |
Weight: | Empty: 29,584 lbs. Combat: 41,547 lbs. Takeoff: 55,923 lbs. | |
Armament: | Eight 20-mm guns with total ammunition of 1280 rounds | |
Engine: | Three J47-GE-13 engines capable of 5,200 lbs. thrust each | |
Takeoff Ground Run: | 4,340 ft. at Sea level, 5,590 ft over 50-ft. obstacle | |
Rate of Climb at Sea Level: | 3,720 (max power) | |
Combat Rate of Climb at Sea Level: | 6,980 (max power) | |
Service Ceiling: | 32,400 ft at takeoff weight under normal power | |
Combat Ceiling: | 38,900 ft at combat weight under max power | |
Average Cruise Speed: | 434 knots | |
Maximum speed: | 500 knots/hour at an optimal altitude of 35,000 ft (combat/max power) | |
Combat Radius: | 378 nautical miles with 4,000 lb. payload at 463 knot average in 1.82 hr. | |
Total Mission Time: | 2.07 hours | |
Crew: | 2 (pilot and shoran operator) | |
Maximum Bombload: | 4 internal bombs (1,600 lb. each) or 2 external bombs (2,000 lb. each) | |
Maximum Bomb Size: | 4,000 | |
Rockets: | Provisions only for (8) 6-in HVAR | |
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