Technical Specifications X-35A/B/C

Powerplant: one Pratt & Whitney F119-611 turbofan probably producing between 34,000 and 40,000 lbs of thrust with afterburning

Dimensions: X-35A: length 50 ft 6 in (15.37m); height ???; wing span 35 ft 0 in (10.65m) X-35C: larger wing span

Weights: unknown

Performance: max level speed unknown; service ceiling probably more than 15,240m (50,000 ft); g limit estimated at +9

Armament: one single-barrel Boeing Advanced 27mm cannon, primary AAM for defense is the AIM-120 AMRAAM of which at least two will be able to be carried in the internal weapon bay. The AIM-9X Sidewinder can only be carried on external additional hardpoints or on the wingtips, not in the internal weapons bay. A large variation of A-G weapons. Of which at least two JDAM GBU-31 (USAF, US Navy requirement) bombs or GBU-32 (USMC requirement) will be able to be carried in the internal weapons bay.