Boeing Company - USA
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Maximum Take-Off Weight
2 x Pratt & Whitney F135 turbofan engines generating up to 43,000lbs of thrust with afterburning.
(2,000 kph | 1,080 knots)
(15,240 m | 9 miles)
(1,575 km | 850 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
1 x 20mm M61A-2 cannon OR 1 x 27mm Mauser BK-27 cannon
Mission-specific ordnance would have included any of the following:
2 OR 6 x AMRAAM air-to-air missiles held in internal bays.
2 x 2,000lb guided bombs held in internal bays in place of four AMRAAM units.
Maximum external loadout was reported to be about 15,000lbs of ordnance.