McDonnell Douglas - USA / Israel Aerospace Industries (IAI) - Israel
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Israel
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
42.8 ft
(13.05 m)
Empty Wgt
31,967 lb
(14,500 kg)
MTOW
81,571 lb
(37,000 kg)
Wgt Diff
+49,604 lb
(+22,500 kg)
(Showcased structural values pertain to the McDonnell Douglas F-15I production variant)
Installed:
2 x Pratt & Whitney F100-PW-229 afterburning turbofan engines developing 14,600lb of dry thrust and 29,150lb of thrust with reheat.
Max Speed
1,656 mph
(2,665 kph | 1,439 kts)
Ceiling
59,711 ft
(18,200 m | 11 mi)
Range
2,485 mi
(4,000 km | 7,408 nm)
Rate-of-Climb
55,000 ft/min
(16,764 m/min)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
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 McDonnell Douglas F-15I 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)
STANDARD, FIXED:
1 x 20mm M61A1 Vulcan Gatling-style internal automatic cannon.
OPTIONAL:
Up to 23,000lb of launched/dropped ordnance including short- and medium-ranged air-to-air missiles, air-to-surface missiles, precision-guided drop bombs, conventional drop bombs, cluster and incendiary bombs, jettisonable fuel tanks, and special-mission equipment (such as targeting pods).
(Not all ordnance types may be represented in the showcase above)
F-15I "Ra am" - Base Series Designation; total of 25 aircraft manufactured.
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