* Specifications(B-1A) *

Primary Function: Long-range, multi-role, heavy bomber

Builder: Rockwell International, North American Aircraft

Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane;
defensive avionics, AIL Division

Power Plant: Four General Electric F-101 GE-100 turbofan engine with afterburner

Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine

Length: 150.2 feet

Wingspan: 136.7 feet extended forward
78.2 feet swept aft

Height: 33.6 feet

Weights: Design Maximum Takeoff: 389,800 lbs.
Design Maximum Ramp: 395,000 lbs.
Maximum Landing: 350,000 lbs.

Speed: Max Speed: at 500 ft. (750 mph)
Max Speed: Mach 2.0 at 50,000 feet (1,320 mph)
Cruise speed: at 50,000 ft (648 mph)

Range: 5,300 miles unrefueled

Ceiling: Over 30,000 feet (9,000 meters)

Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)

Armament: 115,000 lbs
24 AGM-69B SRAM
conventional bombs:75,000 lbs internal plus 40,000 lbs external 32 SRAM

Date Deployed: Cancelled 1977

Unit Cost:

Inventory: none
4 built, 2 crashed and 2 on display