Rockwell B-1 Lancer



Role Supersonic Strategic bomber
National origin United States
Manufacturer North American Rockwell/Rockwell International
Boeing
First flight 23 December 1974
Introduction 1 October 1986
Status In service
Primary user United States Air Force
Produced 1973–1974, 1983-1988
Number built B-1A: 4
B-1B: 100
Unit cost US$283.1 million in 1998 (B-1B)

General characteristics
  • Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
  • Payload: 125,000 lb (56,700 kg) ; internal and external ordnance combined
  • Length: 146 ft (44.5 m)
  • Wingspan:
    • Extended: 137 ft (41.8 m)
    • Swept: 79 ft (24.1 m)
  • Height: 34 ft (10.4 m)
  • Wing area: 1,950 ft² (181.2 m²)
  • Airfoil: NA69-190-2
  • Empty weight: 192,000 lb (87,100 kg)
  • Loaded weight: 326,000 lb (148,000 kg)
  • Max. takeoff weight: 477,000 lb (216,400 kg)
  • Powerplant: 4 × General Electric F101-GE-102 augmented turbofans
    • Dry thrust: 14,600 lbf (64.9 kN) each
    • Thrust with afterburner: 30,780 lbf (136.92 kN) each
  • Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1–3 internal weapons bays each
Performance
Armament
Avionics