|
Dassault Mystere Delta 550
|
1955 |
 |
—Dassault—Aviation—– |
| Aircraft on photo: Dassault Mystere Delta 550 Photo source: Air-defense.net |
|
| |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
1.420 km/h
|
(882 mph)
|
Length: |
Type:
|
experimental interceptor
|
Range: |
NA
|
|
Span:
|
Description:
|
small interceptor jet with delta wings and delta fin |
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1955 |
Ceiling: |
12.000 m
|
(39.370 ft)
|
Max weight: |
| Crew: |
1 |
Climb rate: |
NA |
|
Number built: |
|
12,80 m
|
(42 ft 0 in)
|
7,32 m
|
(24 ft 0 in)
|
4,80 m
|
(15 ft 9 in)
|
5.070 kg
|
(11.177 lb)
|
| 2 |
|
|
Engines:
|
2 x Armstrong Siddeley M.D. 30R Viper turbojets
|
|
|
| Thrust: |
2 x 7,30 kN (2 x 1.640 lbf)
|
|
|
| Armament: |
none
|
|
|
|
|
|
|
|
|
Dassault M.D. 550 Mirage I
|
1956 |
 |
|
| Aircraft on photo: Dassault M.D.550 Mirage I Photo source: Airwar.ru |
|
| |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
1.700 km/h
|
(1.056 mph)
|
Length: |
Type:
|
experimental interceptor
|
Range: |
NA
|
|
Span:
|
Description:
|
Mystere Delta 550 with delta fin changed to
|
Ferry range:
|
NA
|
|
Height:
|
|
sweptback fin, with added rocket engine
|
Ceiling: |
14.600 m
|
(47.900 ft)
|
Max weight: |
|
and renamed as Mirage I |
Climb rate: |
NA |
|
Number built: |
| First flight: |
1956 |
Crew: |
1 |
|
|
|
11,50 m
|
(37 ft 9 in)
|
7,03 m
|
(23 ft 1 in)
|
4,80 m
|
(15 ft 9 in)
|
5.070 kg
|
(11.177 lb)
|
1
|
|
| More info |
/sources: |
|
Engines:
|
2 x Armstrong Siddeley M.D. 30R Viper afterburning turbojets
|
|
|
| |
1 x SEPR liquid-fuel rocket motor
|
|
|
| Thrust: |
2 x 7,30 kN (2 x 1.640 lbf) turbojets dry thrust
|
|
|
| |
2 x 9,61 kN (2 x 2.160 lbf) turbojets with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.300 lbf) rocket engine
|
|
|
| Armament: |
1 x air-to-air missile
|
|
|
|
|
|
|
|
Dassault Mirage III 001 (early version)
|
1956 |
 |
|
| Aircraft on photo: Dassault Mirage III 001 early (prototype) Photo source: Webspace.webring.com |
|
| |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
Mach 1,52
|
|
Length: |
Type:
|
fighter prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage I development with new fuselage |
Ferry range:
|
NA
|
|
Height:
|
|
shape and with single engine |
Ceiling: |
NA
|
|
Gross weight: |
| First flight: |
1956 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
12,80 m
|
(42 ft 0 in)
|
7,58 m
|
(24 ft 10 in)
|
NA
|
|
6.900 kg
|
(15.210 lb)
|
| 1 |
|
More info/
|
sources: |
|
Engine:
|
1 x SNECMA Atar 101G.1 turbojet
|
|
|
| Thrust: |
1 x 44,1 kN (1 x 9.920 lbf) with afterburner
|
|
|
| Armament: |
NA
|
|
|
|
|
| |
|
|
Dassault Mirage III 001 (final version)
|
1957 |
 |
|
| Aircraft on photo: Dassault Mirage III 001 late (prototype) Photo source: Fighters.forumactif.com |
|
| |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
Mach 1,89
|
|
Length: |
Type:
|
fighter prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
modified Mirage III-001 with fixed-geometry lateral |
Ferry range:
|
NA
|
|
Height:
|
|
air intakes replaced by adjustable intake "bullets" |
Ceiling: |
NA
|
|
Gross weight: |
| First flight: |
1957 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
12,80 m
|
(42 ft 0 in)
|
7,58 m
|
(24 ft 10 in)
|
NA
|
|
6.900 kg
|
(15.210 lb)
|
1 (Mirage
|
total 1.422)
|
| |
|
|
Engines:
|
1 x SNECMA Atar 101G.2 turbojet
|
|
|
| |
1 x SEPR 66 rocket motor
|
|
|
| Thrust: |
1 x 44,1 kN (1 x 9.920 lbf) turbojet with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.305 lbf) rocket engine |
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIA
|
1958 |
 |
|
| Aircraft on photo: Dassault Mirage IIIA |
|
| Data for: Mirage IIIA |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.336 km/h
|
(1.450 mph) |
Length: |
Type:
|
interceptor
|
Range: |
1.000 km
|
(620 mi)
|
Span:
|
Description:
|
preproduction aircraft, significantly longer, |
Ferry range:
|
NA
|
|
Height:
|
|
with larger wing and stronger engine |
Ceiling: |
22.500 m
|
(73.820 ft)
|
Max weight: |
| First flight: |
1958 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
14,20 m
|
(46 ft 7 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
9.980 kg
|
(22.000 lb)
|
| 10 |
|
| |
|
|
Engines:
|
1 x SNECMA Atar 9B turbojet
|
|
|
| |
1 x SEPR 844 rocket motor
|
|
|
| Thrust: |
1 x 41,7 kN (1 x 9.370 lbf) turbojet dry thrust
|
|
|
| |
1 x 58,8 kN (1 x 13.230 lbf) turbojet with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.300 lbf) rocket engine |
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIB
|
1959
|
 |
|
| Aircraft on photo: Dassault Mirage IIIBZ |
|
| Data for: Mirage IIIB |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.230 km/h
|
(1.385 mph)
|
Length: |
Type:
|
interceptor-trainer
|
Range: |
580 km
|
(360 mi)
|
Span:
|
Description:
|
two-seat tandem trainer aircraft with |
Ferry range:
|
NA
|
|
Height:
|
|
one piece canopy and without radar |
Ceiling: |
NA
|
|
Max weight: |
| First flight: |
1959 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,39 m
|
(50 ft 5 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
12.000 kg
|
(26.455 lb)
|
| 59 |
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9B-3 turbojet
|
|
|
| Thrust: |
1 x 41,7 kN (1 x 9.370 lbf) dry thrust
|
|
|
| |
1 x 58,8 kN (1 x 13.230 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIC
|
1960 |
 |
|
| Aircraft on photo: Dassault Mirage IIICZ |
|
Data for: Mirage IIIC
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.230 km/h
|
(1.385 mph)
|
Length: |
Type:
|
interceptor-fighter
|
Combat range: |
840 km
|
(520 mi)
|
Span:
|
Description:
|
all-weather interceptor-fighter, half a meter |
Range:
|
1.500 km
|
(930 mi)
|
Height:
|
|
longer then Mirage IIIA and with optional |
Ceiling: |
18.000 m
|
(59.050 ft)
|
Max weight: |
|
rocket engine (which was rarely fitted) |
Climb rate: |
NA |
|
Number built: |
| First flight: |
1960 |
Crew: |
1 |
|
|
|
14,77 m
|
(48 ft 6 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
12.600 kg
|
(27.780 lb)
|
| 95 |
|
More info/
|
sources:
|
|
Engines:
|
1 x SNECMA Atar 9B-3 turbojet
|
|
|
| |
1 x SEPR 841 rocket motor
|
|
|
| Thrust: |
1 x 41,7 kN (1 x 9.370 lbf) turbojet dry thrust
|
|
|
| |
1 x 58,8 kN (1 x 13.230 lbf) turbojet with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.300 lbf) rocket engine |
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIID
|
1966 |
 |
|
| Aircraft on photo: Dassault Mirage IIIDA |
|
Data for: Mirage IIID (similar to Mirage IIIBE and Mirage 5D)
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.450 km/h
|
(1.520 mph)
|
Length: |
Type:
|
fighter-trainer
|
Combat range: |
450 km
|
(280 mi)
|
Span:
|
Description:
|
two-seat trainer version of the Mirage IIIE
|
Range:
|
1.000 km
|
(620 mi)
|
Height:
|
|
with changed nose vs. Mirage IIIB |
Ceiling: |
16.994 m
|
(55.755 ft)
|
Max weight: |
| First flight: |
1966 |
Climb rate: |
61 m/s
|
(12.000 ft/min)
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,39 m
|
(50 ft 5 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
10.200 kg
|
(22.487 lb)
|
| 58 |
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9C turbojet
|
|
|
| Thrust: |
1 x 41,7 kN (1 x 9.370 lbf) dry thrust
|
|
|
| |
1 x 58,8 kN (1 x 13.230 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIE
|
1961
|
 |
|
| Aircraft on photo: Dassault Mirage IIIE |
|
Data for: Mirage IIIE (similar to Mirage 5SDE and Mirage 5EAD)
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
fighter-bomber and strike aircraft
|
Combat range: |
900 km
|
(560 mi)
|
Span:
|
Description:
|
Mirage IIIC with 30 cm fuselage extension |
Range:
|
2.800 km
|
(1.740 mi)
|
Height:
|
|
to make room for the avionics and increase |
Ceiling: |
23.000 m*
|
(74.460 ft)
|
Max weight: |
|
fuel capacity, most of Mirage IIIEs had radar
|
Climb rate: |
NA |
|
Number built: |
|
radom on the fuselage bottom bellow cockpit |
First flight: |
1961 |
|
Crew:
|
|
15,02 m
|
(49 ft 3 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
13.700 kg
|
(30.200 lb)
|
| 523 |
|
| 1 |
|
|
Engines:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| |
1 x SEPR 844 rocket motor
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) turbojet dry thrust
|
|
|
| |
1 x 67,76 kN (1 x 15.235 lbf) turbojet with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.300 lbf) rocket engine |
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIEBR
|
1973 |
 |
|
| Aircraft on photo: Dassault Mirage IIIEBR-2 |
|
| Data for: Dassault Mirage IIIEBR-2 |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
fighter-bomber and strike aircraft
|
Combat range: |
900 km
|
(560 mi)
|
Span:
|
Description:
|
Mirage IIIE with canards modified for
|
Ferry range:
|
2.800 km
|
(1.740 mi)
|
Height:
|
|
Brazilian Air Force |
Ceiling: |
17.000 m
|
(55.775 ft)
|
Max weight: |
| First flight: |
1973; canards upgrade (IIIEBR-2): 1989
|
Climb rate: |
NA |
|
Numb. built: |
| Crew: |
1
|
|
|
|
|
|
15,03 m
|
(49 ft 4 in)
|
8,22 m
|
(27 ft 0 in)
|
4,50 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.200 lb)
|
16
|
|
| |
|
|
Engines:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 67,76 kN (1 x 15.235 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIS
|
1965 |
 |
|
| Aircraft on photo: Dassault Mirage IIIS C70 Photo source: Forum.scramble.nl |
|
Data for: Mirage IIIS C70
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
all-weather interceptor
|
Range: |
2.400 km
|
(1.490 mi)
|
Span:
|
Description:
|
Mirage III for Swiss AF with strengthened |
Ferry range:
|
NA
|
|
Height:
|
|
wings, airframe and undercarriage, |
Ceiling: |
17.000 m*
|
(55.775 ft)
|
Loaded weight: |
|
as of 1988 equipped with canards |
Climb rate: |
83,3 m/s
|
(16.400 ft/min)
|
Number built: |
| First flight: |
1965; canards upgrade (C70): 1988
|
Crew: |
1
|
|
|
|
15,00 m
|
(49 ft 3 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.500 kg
|
(29.760 lb)
|
| 36 |
|
| |
|
|
Engines:
|
1 x SNECMA Atar 9C turbojet
|
|
|
| |
1 x SEPR 844 rocket motor
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) turbojet dry thrust
|
|
|
| |
1 x 60,82 kN (1 x 13.675 lbf) turbojet with afterburner
|
|
|
| |
1 x 14,7 kN (1 x 3.300 lbf) rocket engine |
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIDS / IIIDBR
|
1982 |
 |
|
Aircraft on photo: Dassault Mirage IIIDS/80
|
|
Data for: Mirage IIIDS/80 (similar to Mirage IIIDBR)
|
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.450 km/h
|
(1.520 mph)
|
Length: |
Type:
|
fighter-trainer
|
Comb. range: |
450 km
|
(280 mi)
|
Span:
|
Description:
|
Mirage IIID version for Swiss and Brazil |
Range:
|
1.000 km
|
(620 mi)
|
Height:
|
|
air forces, later upgraded with canards |
Ceiling: |
16.994 m
|
(55.755 ft)
|
Max weight: |
| First flight: |
1982 (DS); canards upgrade (DS/80): 1989 |
Climb rate: |
61 m/s (
|
12.000 ft/min)
|
No built: |
| Crew: |
2 |
|
|
|
|
|
15,39 m
|
(50 ft 5 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
10.200 kg
|
(22.487 lb)
|
2 (DS)
|
|
| 4 (DBR) |
|
|
Engine:
|
1 x SNECMA Atar 9C turbojet
|
|
|
| Thrust: |
1 x 41,7 kN (1 x 9.370 lbf) dry thrust
|
|
|
| |
1 x 58,8 kN (1 x 13.230 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 5
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage IIIT
|
1964 |
 |
|
Aircraft on photo: Dassault Mirage IIIT Photo source: Zonamilitar.com.ar
|
|
| Data for: Dassault Mirage IIIT |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
experimental fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage turbofan engines testbed with rear |
Ferry range:
|
NA
|
|
Height:
|
|
fuselage greater diameter built to support |
Ceiling: |
18.000 m
|
(59.050 ft)
|
Max weight: |
|
Mirage IIIV development |
Climb rate: |
NA
|
|
Number built: |
| First flight: |
1964
|
Crew: |
1
|
|
|
|
14,45 m
|
(47 ft 5 in)
|
8,22 m
|
(27 ft 0 in)
|
4,25 m
|
(13 ft 11 in)
|
10.200 kg
|
(22.487 lb)
|
| 1 |
|
| |
|
|
Engine:
|
1 x SNECMA TF-106 turbofan
|
|
|
| Thrust: |
1 x 88,27 kN (1 x 19.844 lbf) with reheat
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Dassault Mirage IIING
|
1982 |
 |
|
Aircraft on photo: Dassault Mirage IIING Photo source: Forum.keypublishing.com
|
|
| Data for: Mirage IIING |
|
Manufacturer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.440 km/h
|
(1.515 mph)
|
Length: |
Type:
|
multirole fighter
|
Range: |
2.600 km
|
(1.615 mi)
|
Span:
|
Description:
|
modified Mirage 50 prototype with new delta |
Ferry range:
|
NA
|
|
Height:
|
|
wing with leading-edge root extensions, |
Ceiling: |
20.000 m
|
(65.615 ft)
|
Max weight: |
|
fixed canards and fly-by-wire system |
Climb rate: |
NA
|
|
No built: |
| First flight: |
1982
|
Crew: |
1
|
|
|
|
15,09 m
|
(49 ft 6 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
14.700 kg
|
(32.410 lb)
|
| 1 |
|
More info/
|
sources:
|
|
Engine:
|
1 x SNECMA Atar M53 (9K-50) turbojet
|
|
|
| Thrust: |
1 x 70,6 kN (1 x 15.873 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Missiles: 2 x air-to-air, 1 x air-to-ground
|
|
|
|
|
|
|
|
|
Dassault Mirage 5
|
1967
|
 |
|
| Aircraft on photo: Dassault Mirage 5F Photo source: Forum.scramble.nl |
|
| Data for: Mirage 5F |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Combat range: |
1.250 km
|
(777 mi)
|
Span:
|
Description:
|
derived from Mirage III with long slender |
Ferry range:
|
4.000 km
|
(2.485 mi)
|
Height:
|
|
nose as its less expensive version for export |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1967
|
Climb rate: |
186 m/s
|
(36.600 ft/min)
|
No built: |
| Crew: |
1 |
|
|
|
|
|
15,55 m
|
(51 ft 0 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
532 (total
|
Mirage 5)
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9C turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 60,8 kN (1 x 13.688 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
| |
Rockets: 2 x 19 x 68 mm (2 x 19 x 2.68 in)
|
|
|
| |
Missiles: 2 x air-to-air
|
|
|
|
Bombs: 4.000 kg (8.820 lb)
|
|
|
|
Hardpoints: 5
|
|
|
|
|
|
|
|
|
Dassault Mirage 5BA
|
1970 |
 |
|
| Aircraft on photo: Dassault Mirage 5BA |
|
Data for: Mirage 5BA (similar to Mirage 5P)
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Combat range: |
1.300 km
|
(808 mi)
|
Span:
|
Description:
|
Mirage 5 version for Belgium, with |
Ferry range:
|
NA
|
|
Height:
|
|
US avionics and different nose shape |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1970
|
Climb rate: |
186 m/s
|
(36.600 ft/min)
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
15,55 m
|
(51 ft 0 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
63
|
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 60,8 kN (1 x 13.688 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 5BD
|
1970 |
 |
|
| Aircraft on photo: Dassault Mirage 5BD |
|
| Data for: Mirage 5BD |
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
fighter-trainer
|
Combat range: |
NA
|
|
Span:
|
Description:
|
Mirage 5BA trainer version for Belgium, |
Ferry range:
|
NA
|
|
Height:
|
|
with reduced range but combat capable |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1970
|
Climb rate: |
186 m/s
|
(36.600 ft/min)
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
16
|
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 60,8 kN (1 x 13.688 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 5BA MIRSIP / 5MA Elkan
|
1992 |
 |
|
Aircraft on photo: Dassault Mirage 5MA Elkan
|
|
Data for: Mirage 5MA Elkan
|
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Combat range: |
1.300 km
|
(808 mi)
|
Span:
|
Description:
|
Mirage 5BA with canards, modernized to |
Ferry range:
|
2.600 km
|
(1.615 mi)
|
Height:
|
|
MIRSIP standard by SABCA and sold to Chile |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1992
|
Climb rate: |
NA
|
|
No built: |
| Crew: |
1 |
|
|
|
|
|
15,55 m
|
(51 ft 0 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
15
|
|
More info/
|
sources:
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 60,8 kN (1 x 13.688 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 5BD MIRSIP / 5MD Elkan
|
1993 |
 |
|
Aircraft on photo: Dassault Mirage 5BD MIRSIP Photo source: Flyingzone.be
|
|
Data for: Mirage 5MD Elkan
|
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage 5BD with canards and modernized |
Ferry range:
|
NA
|
|
Height:
|
|
to MIRSIP standard |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1993
|
Climb rate: |
186 m/s
|
(36.600 ft/min)
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
5
|
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| |
1 x 60,8 kN (1 x 13.688 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage M5 COAM
|
2001 |
 |
|
Aircraft on photo: Dassault Mirage M5 COAM
|
|
| Data for: Mirage M5 COAM |
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.570 km/h
|
(1.600 mph)
|
Length: |
Type:
|
multirole fighter
|
Range: |
2.600 km
|
(1.615 mi)
|
Span:
|
Description:
|
Mirage 5 development for Columbian Air |
Ferry range:
|
NA
|
|
Height:
|
|
Force with canards, refueling probe and |
Ceiling: |
18.288 m
|
(60.000 ft)
|
Max weight: |
|
different nose, upgraded to Kfir standard |
Climb rate: |
NA
|
|
Number built: |
| First flight: |
2001 |
Crew: |
1 |
|
|
|
15,50 m
|
(50 ft 10 in)
|
8,22 m
|
(27 ft 0 in)
|
4,01 m
|
(13 ft 2 in)
|
13.470 kg
|
(29.700 lb)
|
10
|
|
More info/
|
sources:
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Missiles, Bombs, Rockets |
|
|
|
|
|
|
|
|
Dassault Mirage M5 CODM
|
2001 |
 |
|
Aircraft on photo: Dassault Mirage M5 CODM
|
|
Data for: Mirage M5 CODM
|
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.570 km/h
|
(1.600 mph)
|
Length: |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage M5 COAM trainer version upgraded |
Ferry range:
|
NA
|
|
Height:
|
|
to Kfir standard |
Ceiling: |
18.288 m
|
(60.000 ft)
|
Max weight: |
| First flight: |
2001
|
Climb rate: |
NA
|
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
NA
|
|
8,22 m
|
(27 ft 0 in)
|
NA
|
|
13.470 kg
|
(29.700 lb)
|
2
|
|
More info/
|
sources:
|
|
Engine:
|
1 x SNECMA Atar 9C-3 turbojet
|
|
|
| Thrust: |
1 x 41,97 kN (1 x 9.435 lbf) dry thrust
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50 01
|
1979 |
 |
|
Aircraft on photo: Dassault Mirage 50 01
|
|
Data for: Mirage 50 01
|
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Comb. range: |
630 km
|
(390 mi)
|
Span:
|
Description:
|
Mirage prototype built from Milan with more |
Range:
|
1.300 km
|
(808 mi)
|
Height:
|
|
powerful engine and revised air intakes,
|
Ceiling: |
19.700 m
|
(64.630 ft)
|
Max weight: |
|
designed as economic Mach 2 fighter for exports |
Climb rate: |
186 m/s
|
(36.615 ft/min)
|
No built: |
| First flight: |
1979 |
Crew: |
1 |
|
|
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
14.700 kg
|
(32.407 lb)
|
24 (total
|
Mirage 50)
|
More info/
|
sources:
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50FC
|
1980 |
 |
|
Aircraft on photo: Dassault Mirage 50FC Photo source: Modocharlie.com
|
|
| Data for: Mirage 50FC |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Comb. range: |
630 km
|
(390 mi)
|
Span:
|
Description:
|
Mirage 5F modified to Mirage 50 standard |
Range:
|
1.300 km
|
(808 mi)
|
Height:
|
| First flight: |
1980
|
Ceiling: |
19.700 m
|
(64.630 ft)
|
Max weight: |
| Crew: |
1
|
Climb rate: |
186 m/s
|
(36.615 ft/min)
|
No built: |
|
15,55 m
|
(51 ft 0 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
14.700 kg
|
(32.407 lb)
|
8
|
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50EV
|
1990 |
 |
|
| Aircraft on photo: Dassault Mirage 50EV |
|
| Data for: Mirage 50EV |
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Comb. range: |
690 km
|
(430 mi)
|
Span:
|
Description:
|
upgraded Mirages for Venzuela with stronger |
Range:
|
1.909 km
|
(1.185 mi)
|
Height:
|
|
engine, canards, fuel probe and new avionics |
Ceiling: |
18.288 m
|
(60.000 ft)
|
Max weight: |
| First flight: |
1990
|
Climb rate: |
186 m/s
|
(36.615 ft/min)
|
No built: |
| Crew: |
1 |
|
|
|
|
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,59 m
|
(15 ft 1 in)
|
13.500 kg
|
(29.760 lb)
|
15
|
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50DV
|
1990 |
 |
|
| Aircraft on photo: Dassault Mirage 50DV |
|
| Data for: Mirage 50DV |
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.350 km/h
|
(1.485 mph)
|
Length: |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage 50EV trainer version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1990 |
Ceiling: |
18.288 m
|
(60.000 ft)
|
Max weight: |
| Crew: |
2
|
Climb rate: |
186 m/s
|
(36.615 ft/min)
|
Number built: |
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,59 m
|
(15 ft 1 in)
|
13.500 kg
|
(29.760 lb)
|
3
|
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
Hardpoints capacity: 4.500 kg (9.920 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50CN Pantera
|
1988 |
 |
|
Aircraft on photo: Dassault Mirage 50CN Pantera
|
|
Data for: Mirage 50CN Pantera
|
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.390 km/h
|
(1.485 mph)
|
Length: |
Type:
|
multirole fighter
|
Comb. range: |
685 km
|
(425 mi)
|
Span:
|
Description:
|
Mirage version upgraded by ENAER to the |
Ferry range:
|
2.400 km
|
(1.490 mi)
|
Height:
|
|
Kfir C-2 look with canards, extended nose
|
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
|
and new avionics |
Climb rate: |
NA
|
|
No built: |
| First flight: |
1988 |
Crew: |
1 |
|
|
|
15,56 m
|
(51 ft 1 in)
|
8,22 m
|
(27 ft 0 in)
|
4,5 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
14
|
|
More info
|
/sources:
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 4 |
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 50DC Pantera
|
1993
|
 |
|
Aircraft on photo: Dassault Mirage 50DC Pantera
|
|
Data for: Mirage 50DC Pantera
|
|
Manufacturer:
|
Dassault Aviation, France |
Max speed:
|
2.390 km/h
|
(1.460 mph)
|
Length (pitot inc.): |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
Mirage Pantera trainer version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1993 (estimate)
|
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| Crew: |
2
|
Climb rate: |
NA
|
|
Number built: |
|
16,91 m
|
(55 ft 6 in)
|
8,22 m
|
(27 ft 0 in)
|
4,50 m
|
(14 ft 9 in)
|
13.700 kg
|
(30.203 lb)
|
2
|
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 4 |
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage F1 01
|
1966 |
 |
|
Aircraft on photo: Dassault Mirage F1 01
|
|
(also called Mirage F1C)
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed (est):
|
Mach 2
|
|
Length: |
Type:
|
fighter prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
first Mirage F.1 prototype with Mirage IIIE nose |
Ferry range:
|
NA
|
|
Height:
|
|
which crashed only 5 months after first flight |
Ceiling: |
NA
|
|
Max weight: |
| First flight: |
1966
|
Climb rate: |
NA
|
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
NA
|
|
8,40 m
|
(27 ft 7 in)
|
4,50 m
|
(14 ft 9 in)
|
NA
|
|
1
|
|
| |
|
|
Engine:
|
1 x SNECMA Atar 9K-31 turbojet
|
|
|
| Thrust: |
1 x 65,7 kN (1 x 14.770 lbf) with afterburner |
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Dassault Mirage F1
|
1966 |
 |
|
Aircraft on photo: Dassault Mirage F1CE(M)
|
|
Data for: Mirage F1C
|
|
Manufacturer:
|
Avions Marcel Dassault, France |
Max speed:
|
2.350 km/h
|
(1.460 mph)
|
Length: |
Type:
|
multirole fighter
|
Comb. range: |
660 km
|
(410 mi)
|
Span:
|
Description:
|
scaled-down Mirage F2 version, single-seat |
Range:
|
900 km
|
(559 mi)
|
Height:
|
|
fighter with conventional sweptback wing
|
Ceiling: |
20.000 m
|
(65.615 ft)
|
Max weight: |
| First flight: |
1966 (prototype)
|
Climb rate: |
168 m/s
|
(33.000 ft/min)
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
15,25 m
|
(55 ft 6 in)
|
8,44 m
|
(27 ft 8 in)
|
4,50 m
|
(14 ft 9 in)
|
16.200 kg
|
(35.715 lb)
|
731 (total
|
Mirage F1)
|
| More info/ |
sources: |
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 4 x underwing, 1 x centerline, 2 x wingtip |
|
|
|
Hardpoints capacity: 4.700 kg (10.360 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage F1.M53
|
1974 |
 |
|
Aircraft on photo: Dassault Mirage F1.M53 Photo source: Flickr by aerofifties
|
|
| (also called: Mirage F1E.M53) |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.335 km/h
|
(1.450 mph)
|
Length: |
Type:
|
fighter prototype
|
Range: |
1.200 km
|
(745 mi)
|
Span:
|
Description:
|
Mirage F1 with more power, longer fuselage, |
Fer. range:
|
NA
|
|
Height:
|
|
increased fuel capacity, enlarged air intakes
|
Ceiling: |
NA
|
|
Take off weight: |
|
and strengthened undercarriage; lost compe-
|
Climb rate: |
NA
|
|
Number built: |
|
tition for European F-104 successor to F-16 |
First flight: |
1974 |
|
Crew:
|
|
15,48 m
|
(50 ft 9 in)
|
8,45 m
|
(27 ft 9 in)
|
4,56 m
|
(15 ft 0 in)
|
15.200 kg
|
(33.510 lb)
|
1
|
|
1
|
|
|
Engine:
|
1 x SNECMA M53 turbojet
|
|
|
| Thrust: |
1 x 54,4 kN (1 x 12.235 lbf) dry thrust
|
|
|
| |
1 x 83,4 kN (1 x 18.740 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 7 |
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage F1A
|
1975 |
 |
|
| Aircraft on photo: Dassault Mirage F1AZ |
|
| Data for: Mirage F1AZ |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.335 km/h
|
(1.450 mph)
|
Length: |
Type:
|
strike and multirole fighter
|
Range: |
1.800 km
|
(1.200 mi)
|
Span:
|
Description:
|
Mirage F1 with slender conical nose and pitot |
Ferry range:
|
NA
|
|
Height:
|
|
underside as a result of substituting large Cyrano
|
Ceiling: |
20.000 m
|
(65.615 ft)
|
Max weight: |
|
radar with ranging radar and laser-ranger |
Climb rate: |
168 m/s
|
(33.000 ft/min)
|
No built: |
| First flight: |
1975 |
Crew: |
1 |
|
|
|
15,00 m
|
(49 ft 3 in)
|
8,40 m
|
(27 ft 7 in)
|
4,50 m
|
(14 ft 9 in)
|
16.200 kg
|
(35.700 lb)
|
32 (F1AZ);
|
16 (F1AD)
|
|
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,3 kN (1 x 11.090 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
| |
Hardpoints capacity: 4.000 kg (8.820 lb) |
|
|
|
Bombs, Cluster munitions, Missiles, Rocket launchers |
|
|
|
|
|
|
|
|
Dassault Mirage F1B / F1D
|
1976 |
 |
|
| Aircraft on photo: Dassault Mirage F1B |
|
| Data for: Mirage F1B |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.335 km/h
|
(1.450 mph)
|
Length: |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
2-seat Mirage F1 trainer version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1976
|
Ceiling: |
20.000 m
|
(65.615 ft)
|
Max weight: |
| Crew: |
2
|
Climb rate: |
168 m/s
|
(33.000 ft/min)
|
No built: |
|
15,53 m
|
(50 ft 11 in)
|
8,40 m
|
(27 ft 7 in)
|
4,50 m
|
(14 ft 9 in)
|
16.200 kg
|
(35.715 lb)
|
57 (F1B);
|
4 (F1D)
|
|
Engine:
|
1 x SNECMA Atar 9K-50 turbojet
|
|
|
| Thrust: |
1 x 49,0 kN (1 x 11.025 lbf) dry thrust
|
|
|
| |
1 x 70,6 kN (1 x 15.875 lbf) with afterburner
|
|
|
| Armament: |
Guns: external cannon pods
|
|
|
|
Hardpoints capacity: 4.000 kg (8.820 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 2000
|
1978
|
 |
|
| Aircraft on photo: Dassault Mirage 2000C |
|
| Data for: Mirage 2000C |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.530 km/h
|
(1.500 mph)
|
Length: |
Type:
|
multirole fighter
|
Range: |
1.550 km*
|
(963 mi)
|
Span:
|
Description:
|
lightweight fourth-generation fighter based on |
Ferry range:
|
3.335 km**
|
(2.073 mi)
|
Height:
|
|
Mirage III and developed for French Air Force |
Ceiling: |
17.060 m
|
(59.000 ft)
|
Max weight: |
| First flight: |
1978
|
Climb rate: |
285 m/s
|
(56.000 ft/min)
|
No built: |
| Crew: |
1 |
|
|
|
|
|
14,36 m
|
(47 ft 1 in)
|
9,13 m
|
(29 ft 11 in)
|
5,20 m
|
(17 ft 1 in)
|
17.000 kg
|
(37.500 lb)
|
601 (total
|
Mirage 2000)
|
|
|
|
Engine:
|
1 x SNECMA M53-P2 afterburning turbofan
|
|
* with drop tanks |
| Thrust: |
1 x 64,3 kN (1 x 14.500 lbf) dry thrust
|
|
** with auxiliary fuel |
| |
1 x 95,1 kN (1 x 21.400 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
|
Hardpoints: 9 (4 x under wing, 5 x under fuselage) |
|
|
|
Hardpoints capacity: 6.300 kg (13.900 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 2000B
|
1980
|
 |
|
| Aircraft on photo: Dassault Mirage 2000B |
|
| Data for: Mirage 2000B |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.340 km/h
|
(1.454 mph)
|
Length: |
Type:
|
fighter-trainer
|
Range: |
1.650 km*
|
(1.025 mi)
|
Span:
|
Description:
|
Mirage 2000 two-seat trainer version |
Ferry range:
|
3.335 km**
|
(2.073 mi)
|
Height:
|
| First flight: |
1980 |
Ceiling: |
16.460 m
|
(54.000 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
285 m/s
|
(56.000 ft/min)
|
No built: |
|
14,55 m
|
(47 ft 9 in)
|
9,13 m
|
(29 ft 11 in)
|
5,15 m
|
(16 ft 11 in)
|
17.000 kg
|
(37.500 lb)
|
78 (total
|
trainers)
|
|
Engine:
|
1 x SNECMA M53-P2 afterburning turbofan
|
|
|
| Thrust: |
1 x 64,3 kN (1 x 14.500 lbf) dry thrust
|
|
* with drop tanks |
| |
1 x 95,1 kN (1 x 21.400 lbf) with afterburner
|
|
** with auxiliary fuel |
| Armament: |
Guns: 30 mm (1.18 in) in external cannon pod
|
|
|
|
Hardpoints: 9 (4 x under wing, 5 x under fuselage) |
|
|
|
Hardpoints capacity: 6.300 kg (13.900 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 2000N
|
1986
|
 |
|
| Aircraft on photo: Dassault Mirage 2000N |
|
| Data for: Mirage 2000N |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.338 km/h
|
(1.453 mph)
|
Length: |
Type:
|
nuclear strike fighter-bomber
|
Range: |
1.480 km
|
(920 mi)
|
Span:
|
Description:
|
designed to replace Mirage IVP, forms the core |
Ferry range:
|
3.340 km
|
(2.075 mi)
|
Height:
|
|
of the French air-based tactical nuclear deterrent |
Ceiling: |
18.000 m
|
(59.055 ft)
|
Max weight: |
| First flight: |
1986
|
Climb rate: |
285 m/s
|
(56.000 ft/min)
|
No built: |
| Crew: |
2 |
|
|
|
|
|
14,55 m
|
(47 ft 9 in)
|
9,13 m
|
(29 ft 11 in)
|
5,15 m
|
(16 ft 11 in)
|
17.000 kg
|
(37.500 lb)
|
75
|
|
|
|
|
Engine:
|
1 x SNECMA M53-P2 afterburning turbofan
|
|
|
| Thrust: |
1 x 64,3 kN (1 x 14.500 lbf) dry thrust
|
|
|
| |
1 x 95,1 kN (1 x 21.400 lbf) with afterburner
|
|
|
| Armament: |
Guns: 30 mm (1.18 in) in external cannon pod |
|
|
|
Hardpoints: 9 (4 x under wing, 1 x centerline, 4 x under fuselage) |
|
|
|
Hardpoints capacity: 6.300 kg (13.900 lb)
|
|
|
|
|
|
|
|
|
Dassault Mirage 4000
|
1979
|
 |
|
Aircraft on photo: Dassault Mirage 4000 Photo source: Scenicreflections.com
|
|
| Data for: Mirage 4000 |
|
Producer:
|
Avions Marcel Dassault-Breguet Aviation, France |
Max speed:
|
2.445 km/h
|
(1.519 mph)
|
Length: |
Type:
|
prototype fighter aircraft
|
Range: |
2.000 km
|
(1.200 mi)
|
Span:
|
Description:
|
scaled-up and twin engined version of the |
Ferry range:
|
NA
|
|
Height:
|
|
Mirage 2000 designed to compete with F-15 |
Ceiling: |
20.000 m
|
(66.000 ft)
|
Max weight: |
| First flight: |
1979
|
Climb rate: |
305 m/s
|
(60.040 ft/min)
|
No built: |
| Crew: |
1 |
|
|
|
|
|
18,70 m
|
(61 ft 4 in)
|
12,00 m
|
(39 ft 4 in)
|
5,80 m
|
(19 ft 0 in)
|
32.000 kg
|
(70.550 lb)
|
1
|
|
| More info/ |
sources:
|
|
Engines:
|
2 x SNECMA M53-P2 afterburning turbofans
|
|
|
| Thrust: |
2 x 64,3 kN (2 x 14.500 lbf) dry thrust
|
|
|
| |
2 x 95,1 kN (2 x 21.400 lbf) with afterburner
|
|
|
| Armament: |
Guns: 30 mm (1.18 in) in external cannon pod |
|
|
|
Hardpoints: 13 (6 x under wing, 7 x under fuselage) |
|
|
|
Hardpoints capacity: 8.000 kg (17.640 lb)
|
|
|
|
|
|
|
|
| |
|
