Mitsubishi Heavy Industries (MHI) - Japan / McDonnell Douglas; Boeing - USA
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(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Mitsubishi F-15J production variant)
2 x Pratt & Whitney F100-100 OR F100-200 afterburning turbofan engines developing 17,450lb of thrust (each) dry and 25,000lb of thrust (each) with reheat.
(2,665 kph | 1,439 kts)
(20,000 m | 12 mi)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the Mitsubishi F-15J production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
1 x 20mm M61 "Vulcan" Gatling-style rotary automatic internal cannon.
OPTIONAL, ROLE DEPENDENT:
Support for various in-service Japanese and American Air-to-Air Missiles (AAMs) including AAM-3, AAM-4, AAM-5, AIM-9 "Sidewinder", and AIM-7 "Sparrow".
For ground support roles, provision for Mk 82 family of General Purpose Bombs (conventional drop bombs), the CBU-87 Cluster bomb and others.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.