B-1A
| Specifications | |
|---|---|
| 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: |
| Date Deployed: | Cancelled 1977 |
| Unit Cost: | |
| Inventory: | none 4 built, 2 crashed and 2 on display |
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
