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Bomber

B-1B Lancer

Rockwell · USA

The B-1B "Bone" was optimized for low-level penetration of Soviet airspace. It featured a significantly reduced radar cross-section (RCS) compared to the B-1A and carried a massive internal payload of conventional or nuclear munitions.

Technical Specifications
First Flight 1983
Max Speed 1,335 km/h (Mach 1.25)
Range 9,400 km
Ceiling 18,000 m
Engines 4x General Electric F101-GE-102 afterburning turbofans
Armament & Payload

Up to 34,000 kg of internal ordnance across three bays.