DASSAULT Mirage F1

Aircraft
Name: 
Mirage F1
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Tail: 
Regular tail, mid set
WTC
M
APC
C
Type Code: 
L1J
Engine: 
Jet
Engine Count: 
Single
Position: 
In fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
DASSAULT Mirage F1

MRF1

Multi-role fighter. In service since 1973. Improved development of Mirage 3 with advanced technology and swept wings. Different versions for intercept, attack and reconnaissance role. Production ended in 1989.

Technical Data
Wing span: 
8.40 m
Length: 
15.00 m
Height: 
4.50 m
Powerplant: 

1 x 72.0 kN reheated SNECMA ATAR 9k-50 afterburning turbojet.

Engine Model: 
SNECMA Atar 9
Indicative Performance Data
Take-Off
V2: 
140 kts
Distance: 
700 m
MTOW: 
15200 kg
Initial Climb (to 5000 ft)
IAS: 
170 kts
ROC: 
40000 ft/min
Initial Climb (to FL150)
IAS: 
300 kts
ROC: 
30000
Initial Climb (to FL240)
IAS: 
300 kts
ROC: 
20000 ft/min
MACH Climb
MACH: 
0.80
ROC: 
15000 ft/min
Cruise
TAS: 
525 kts
MACH: 
0.86
Ceiling: 
650
Range: 
1000 NM
Initial Descent (to FL240)
MACH: 
0.85
ROD: 
20000 ft/min
Descent (to FL100)
IAS: 
400 kts
ROD: 
10000 ft/min
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
145 kts
Distance: 
600 m

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