Credit
MSgt Eric Harris · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Mirage F1 · Length
Single source15.3 m (50 ft 2 in)[source]
F-15E · Length
Single sourceConfiguration
| Specification | Dassault Mirage F1 | McDonnell Douglas F-15E Strike Eagle |
|---|---|---|
| Type | Fighter aircraft[source] | Multirole strike fighter[source] |
| National origin | France[source] | United States[source] |
| Manufacturer | Dassault Aviation[source] | McDonnell Douglas (1985–1997) Boeing Defense, Space & Security (1997–2017)[source] |
| Status | In limited service[source] |
63 ft 9.6 in (19.446 m)[source]
Empty; Mirage F1 · Empty weight
Single sourceGross; Mirage F1 · clean take-off weight
Single sourceMaximum take-off; Mirage F1 · Max takeoff weight
Single source7,400 kg (16,314 lb)[source]
10,900 kg (24,030 lb) (clean take-off weight)[source]
16,200 kg (35,715 lb)[source]
Empty; F-15E · or
Single sourceEmpty; F-15E · with CFTs
Single sourceMaximum; Mirage F1 · at 11,000 m (36,000 ft)
Single source2,338 km/h (1,453 mph, 1,262 kn) at 11,000 m (36,000 ft)[source]
Maximum; F-15E · at low altitude
Single sourceMaximum; F-15E · Mach 2.5 at high altitude Mach 1.2
Single sourceMach 2.5, 1,650 mph (2,655 km/h) at high altitude Mach 1.2, 800 kn (921 mph; 1,482 km/h) at low altitude[source]
Ferry; Mirage F1 · with maximum external fuel
Single source3,300 km (2,100 mi, 1,800 nmi) with maximum external fuel[source]
Ferry; F-15E · with conformal fuel tanks and three external fuel tanks
Single source2,100 nmi (2,400 mi, 3,900 km) with conformal fuel tanks and three external fuel tanks[source]
Mirage F1 · 1 × SNECMA Atar 9K-50 afterburning turbojet engine thrust dry
Single sourceMirage F1 · with afterburner
Single source1 × SNECMA Atar 9K-50 afterburning turbojet engine, 49.03 kN (11,020 lbf) thrust dry, 70.6 kN (15,900 lbf) with afterburner[source]
F-15E · ); 29,160 lb (
Single sourceF-15E · 2 × Pratt & Whitney F100-PW-220 afterburning turbofan thrust each dry
Single sourceMirage F1 · combat air patrol, with 2 × Super 530 missiles and centreline drop tank
Single source2 hr 15 min (combat air patrol, with 2 × Super 530 missiles and centreline drop tank)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Primary users | French Air Force (historical) Iraqi Air Force (historical) Hellenic Air Force (historical) Spanish Air Force (historical)[source] | United States Air Force Royal Saudi Air Force Israeli Air Force Republic of Korea Air Force For other users, see Operators[source] |
|---|
| Number built | 726[source] | 435 (F-15E/I/S/K/SG)[source] |
|---|
| Manufactured | 1966–1992[source] | 1985–2017[source] |
|---|
| Introduction date | 1973 ( 1973 )[source] | 1988 30 September 1989 ( IOC )[source] |
|---|
| First flight | 23 December 1966 ( 1966-12-23 )[source] | 11 December 1986 ( 1986-12-11 )[source] |
|---|
| Developed from | Dassault Mirage III[source] | McDonnell Douglas F-15 Eagle[source] |
|---|
| Guns | 2× 30 mm (1.18 in) DEFA 553 cannons with 150 rounds per gun[source] | 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled rotary cannon , 500 rounds of either M-56 or PGU-28 ammunition[source] |
|---|
| Hardpoints | 1 centreline pylon, four underwing and two wingtip pylons with a capacity of 6,300 kg (13,900 lb) (practical maximum load 4,000 kg (8,800 lb)), with provisions to carry combinations of: Rockets: 8× Matra rocket pods with 18× SNEB 68 mm rockets each Bombs: various Other: reconnaissance pods or Drop tanks[source] | 4 wing pylons, fuselage pylons, bomb racks on CFTs with a capacity of 23,000 lb (10,400 kg) of external fuel and ordnance[source] |
|---|
| Thrust/weight | 0.66[source] | 0.93[source] |
|---|
| Rockets | 8× Matra rocket pods with 18× SNEB 68 mm rockets each[source] | — |
|---|
| Bombs | various[source] | Mark 82 bomb Mark 84 bomb GBU-15 GBU-10 Paveway II GBU-12 Paveway II GBU-24 Paveway III GBU-27 Paveway III GBU-28 (Bunker buster) GBU-31 or GBU-38 {8 GBU-31s or 16 GBU-38s} (JDAM) GBU-54 Laser JDAM (LJDAM) GBU-39 Small Diameter Bomb (SDB) B61 nuclear bomb CBU-87 or CBU-103 (CEM) CBU-89 or CBU-104 (GATOR) KGGB (integrated on South Korean Air Force F-15Ks) CBU-97 or CBU-105 (SFW) CBU-107 Passive Attack Weapon BLU-107 Durandal[source] |
|---|
| Other | reconnaissance pods or Drop tanks[source] | — |
|---|
| Missiles | 2× AIM-9 Sidewinders OR Matra R550 Magics on wingtip pylons, 2× R.530 or Super 530 Fs underwing, 1× AM-39 Exocet anti-ship missile, 2× AS-30L laser-guided missiles[source] | Air-to-air missiles : 4× AIM-7 Sparrow 4× AIM-9 Sidewinder or IRIS-T (S variant of the Saudi Air Force ) 8× AIM-120 AMRAAM Air-to-surface missiles : 6× AGM-65 Maverick 2× AGM-84 Harpoon 2× AGM-84H/K SLAM-ER 2x AGM-130 AGM-154 JSOW AGM-158 JASSM Joint Strike Missile (to be integrated) Taurus KEPD 350 (integrated on South Korean Air Force F-15Ks)[source] |
|---|
| Alternative designation | Mirage F1[source] | — |
|---|
| Variant | — | Boeing F-15SE Silent Eagle[source] |
|---|
| Developed into | — | Boeing F-15EX Eagle II[source] |
|---|
| Fuel capacity | — | 12,915 lb (5,858 kg) internal, 22,267 lb (10,100 kg) with CFTs, 34,162 lb (15,496 kg) with CFTs and 3× 600-gallon (2,270 L) external fuel tanks[source] |
|---|
| Airfoil | — | root: NACA 64A006.6 ; tip: NACA 64A203[source] |
|---|
| g limits | — | + 9[source] |
|---|
| Others | — | up to 3× 600 US gallons (2,300 L ) external drop tanks for ferry flight or extended range/loitering time 3 x 7-round (21) APKWS under each wing[source] |
|---|
| Radar | — | Raytheon AN/APG-70 or AN/APG-82 AN/ASQ-236 Radar Pod[source] |
|---|
| Targeting pods | — | AN/AAQ-14 LANTIRN or Lockheed Martin Sniper XR or AN/AAQ-28(V) Litening[source] |
|---|
| Countermeasures | — | Northrop Grumman Electronic Systems AN/ALQ-131 electronic countermeasures pod Hazeltine AN/APX-76 or Raytheon AN/APX-119 Identify Friend/Foe (IFF) interrogator Magnavox AN/ALQ-128 Electronic Warfare Warning Set (EWWS) – part of Tactical Electronic Warfare Systems (TEWS) Loral AN/ALR-56 Radar warning receivers (RWR) – part of TEWS Northrop Grumman Electronic Systems ALQ-135 Internal Countermeasures System (ICS) – part of TEWS Marconi AN/ALE-45 Chaff / Flares dispenser system – part of TEWS BAE Systems AN/ALQ-250 Eagle Passive Active Warning Survivability System (EPAWSS) - combined electronic warfare / electronic countermeasures system[source] |
|---|
Maximum take-off; F-15E · Max takeoff weight
Single sourceF-15E · ) with afterburner each
Single sourceF-15E · with afterburner ( or 2 × F100-PW-229 , thrust: 17,800 lb dry (
Single source2 × Pratt & Whitney F100-PW-220 afterburning turbofan , 14,590 lbf (64.9 kN) thrust each dry, 23,770 lbf (105.7 kN) with afterburner ( or 2 × F100-PW-229 , thrust: 17,800 lb dry (79 kN); 29,160 lb (129.7 kN) with afterburner each)[source]