DASSAULT Mirage 2000 Vajra

Aircraft
Name: 
Mirage 2000 Vajra
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Delta wing
Tail: 
No tail plane
WTC
M
APC
C
Type Code: 
L1J
Engine: 
Jet
Engine Count: 
Single
Position: 
In fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
DASSAULT Mirage 2000
DASSAULT Vajra

MIR2

Multi-role nuclear and conventional strike fighter. In service since 1983. Mirage 2000 combines the benefits of the delta wing layout with fly-by-wire technology. Developed in several versions: Mirage 2000B two seat trainer, 2000N-K1/K2 nuclear strike version (first flight 3. Feb. 1983) and 2000D (export 2000N-KL) conventional strike fighter (first flight 19. Feb. 1991). Latest model 2000-9 exported to several countries as well as being used by French Air Force.

Technical Data
Wing span: 
9.10 m
Length: 
14.40 m
Height: 
5.20 m
Powerplant: 

1 x 95,1 kN SNECMA M53 - P2 afterburning turbofan.

Engine Model: 
SNECMA M53
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
17000 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
56000 ft/min
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
800 kts
MACH: 
2.20
Ceiling: 
590
Range: 
1800 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
140 kts
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
140 kts
Distance: 
n/a

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