MG23
MIKOYAN MiG-23 Bahadur
MIKOYAN MiG-23 Bahadur
Aircraft
Name
MiG-23 Bahadur
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High swing wing
Tail
Regular tail, high set
WTC
M
APC
C
Type Code
L1J
Engine
Jet
Engine Count
Single
Position
In fuselage
Landing gear
Tricycle retractable
Manufactured as
MIKOYAN MiG-27
MIKOYAN Bahadur
MIKOYAN MiG-23
MIKOYAN MiG-27 Bahadur
HINDUSTAN Bahadur
HINDUSTAN MiG-27 Bahadur
MG23
Technical Data
Wing span (metric)
14.00 m
Length (metric)
15.90 m
Height (metric)
4.80 m
Powerplant
MiG-23: 1 x 127,5 KN Tumansky R-35-300 afterburning turbojets.
Indicative Performance Data
Take-Off
V2
n/a
Distance
800 m
MTOW
20700 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
39000 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
n/a
MACH
1.77
Ceiling
460
Range
944 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
950 m
