The Rockwell B-1B Lancer
USA, Strategic heavy bomber
Specifications:
Rockwell B-1B Lancer
Powerplant: four General Electric F101-GE-102 turbofans each rated at 64.94 kN dry and 136.92 kN with afterburning
Dimensions: wing span 41.67 m (15¡Æ) and 23.84 m (67¡Æ 30'); length 44.81 m ; height 10.36 m ;wing area approximately 181.16 m2
Weights: empty equipped 87 091 kg ; maximum take-off 216 365 kg
Performance: maximum level speed "clean" at high altitude about Mach 1.25 or 715 kt (1324 km/h); penetration speed at 61 m more than 521 kt (965 km/h); range 6475 nm (12 000 km) with standard fuel
Armament: internal maximum payload of 34 020 kg, including AGM-9A SRAM-A's; B-28, B-61 or B-83 free-fall nuclear bombs; AGM-86B ALCM's (and possibly AGM-129A ACM's); 84 227-kg Mk 82 bombs or 227-kg Mk 36 mines internally, AGM-86C ALCM's armed with a 454-kg blast fragmentation warhead
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