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
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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