PERFORMANCE ANALYSIS - Checksix MIG-21M iz.96A-NFM ... Mikoyan-Gourevitch Corporation (Tumanskiy...
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A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6 Mig-21M iz.96A / L-15 Mikoyan-Gourevitch Corporation (Tumanskiy R-11F2SK-200) PERFORMANCE ANALYSIS CAUTION STATEMENT : This document is to be use only for simulation. Do not try to apply the procedures and or advices contained in it if you have the opportunity to fly this plane in real life. By the way, if you had (or still have) flew this aircraft, your comments, criticism and more are welcome I – 1 - 1 LICENSE : This document has been created by J.M. LANGERON / TOPOLO, (http://topolo.free.fr/) all the values used to model the aircraft behavior have been computed by him, like all performance charts presented here. If you want to use these data, or part of it, please contact the author by personal message to TOPOLO on check-six forum: (http://www.checksix-forums.com/)
Transcript of PERFORMANCE ANALYSIS - Checksix MIG-21M iz.96A-NFM ... Mikoyan-Gourevitch Corporation (Tumanskiy...
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
Mig-21M iz.96A / L-15
Mikoyan-Gourevitch Corporation
(Tumanskiy R-11F2SK-200)
PERFORMANCE ANALYSIS
CAUTION STATEMENT : This document is to be use only for simulation. Do not try to apply the procedures and or advices contained in it if
you have the opportunity to fly this plane in real life. By the way, if you had (or still have) flew this aircraft, your comments, criticism and
more are welcome
I – 1 - 1
LICENSE : This document has been created by J.M. LANGERON / TOPOLO, (http://topolo.free.fr/) all the values used to model the aircraft
behavior have been computed by him, like all performance charts presented here. If you want to use these data, or part of it, please contact the
author by personal message to TOPOLO on check-six forum: (http://www.checksix-forums.com/)
Level Flight Envelope
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 2
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
50,000
55,000
60,000
65,000
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Alt
(ft
)
Mach
Level Flight EnveloppeMIL Power
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
50,000
55,000
60,000
65,000
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Alt
(ft
)
Mach
Level Flight EnveloppeFull AB
Level Flight Envelope
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MILL Power
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
2 x R-3S
GW = 15,773 lbs
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 3
2 x R-3S +
CL Tank 490l
GW = 16,255 lbs
700 Kts / 1,300 Km/h
(IAS)
2 x R-3S
GW = 15,773 lbs
2 x R-3S +
CL Tank 490l
GW = 16,255 lbs700 Kts / 1,300 Km/h
(IAS)
Turn Performance
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•50% internal fuel
•GW= 15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 4
0.00
5.00
10.00
15.00
20.00
25.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Maxim
um
in
sta
nta
neo
us tu
rn r
ate
(d
eg
/s)
Mach number
Maximum Available Turn Rate
0
10,000
20,000
30,000
40,000
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 5
Maximum reached without AoA limit
(Stall speed)
Ng < 8 for mach number < 0.8
Ng < 6 for mach number > 0.8
0.00
5.00
10.00
15.00
20.00
25.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Su
sta
ine
d T
urn
ra
te (d
eg
/s)
Mach number
Maximum Sustained Turn rate (deg/s)
0
10,000
20,000
30,000
40,000
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Ma
xim
um
Av
aila
ble
Lo
ad
Fa
cto
r (N
g)
Mach number
Maximum Available Load Factor
0
10,000
20,000
30,000
40,000
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 6
Maximum reached without AoA limit
(Stall speed)
Ng < 8 for mach number < 0.8
Ng < 6 for mach number > 0.8
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
Mach number
Maximum Sustained Load Factor (Ng)
0
10,000
20,000
30,000
40,000
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Max. Sustained Turn = 11.5 deg/s
+100
0
-100
-300
+200
9G8G7G6G5G4G3G2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Quickest Turn = 22.6 deg/s
MA
XIM
UM
AIR
SP
EE
D
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
-200
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 7
+300
Quickest Turn = 18.9 deg/s
Maximum
allowed
AoA (28)
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
+100
0
-100
-200
-300
+200
9G8G7G6G5G4G3G2G
Turn Performance – 5,000 ft
Quickest Turn = 20.7 deg/s
Max. Sustained Turn = 10.6 deg/s
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 8
+300
Quickest Turn = 17.7 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 9
+100
0
-100
-200
-300
+200
9G8G7G6G5G4G3G2G
Quickest Turn = 15.9 deg/s
Max. Sustained Turn = 9.8 deg/s
Quickest Turn = 18.9 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
+300
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 10
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 13.2 deg/s
Max. Sustained Turn = 8.9 deg/s
+200
+300
Quickest Turn = 17.1 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 11
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 14.2 deg/s
Max. Sustained Turn = 7.5 deg/s
+200
+300
Quickest Turn = 12.0 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 12
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 12.50 deg/s
Max. Sustained Turn = 6.4 deg/s
+200
Quickest Turn = 11.5 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 13
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 11.3 deg/s
Max. Sustained Turn = 5.3 deg/s
+200
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 10.7 deg/s
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 14
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 9.3 deg/s
Max. Sustained Turn = 4.6 deg/s
+200
+100
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 10.0 deg/s
Climb Performance
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 15
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•50% internal fuel
•GW= 15,673 lbs / 7,100 kg
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 16
0
100
200
300
400
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 17
0
100
200
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Acceleration Performances
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 18
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•50% internal fuel
•GW= 15,673 lbs / 7,100 kg
0
15
30
45
60
75
90
105
120
135
150
165
180
0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
30,000 30,000 36,000
0
15
30
45
60
75
90
105
120
135
150
165
180
0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
0 10,000 20,000
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 12 (2xR-3S)
•GW=15,673 lbs / 7,100 kg
Sea Level
10,000 ft
30,000 ft
36,000 ft
30,000 ft
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 19
20,000 ft
Turn Performance
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•50% internal fuel
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 20
0.00
5.00
10.00
15.00
20.00
25.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Maxim
um
in
sta
nta
neo
us tu
rn r
ate
(d
eg
/s)
Mach number
Maximum Available Turn Rate
0
10,000
20,000
30,000
40,000
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 21
Maximum reached without AoA limit
(Stall speed)
Ng < 7 for mach number < 0.8
Ng < 6 for mach number > 0.8
0.00
5.00
10.00
15.00
20.00
25.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Su
sta
ine
d T
urn
ra
te (d
eg
/s)
Mach number
Maximum Sustained Turn rate (deg/s)
0
10,000
20,000
30,000
40,000
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Ma
xim
um
Av
aila
ble
Lo
ad
Fa
cto
r (N
g)
Mach number
Maximum Available Load Factor
0
10,000
20,000
30,000
40,000
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 22
Maximum reached without AoA limit
(Stall speed)
Ng < 7 for mach number < 0.8
Ng < 6 for mach number > 0.8
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20 2.40
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
Mach number
Maximum Sustained Load Factor (Ng)
0
10,000
20,000
30,000
40,000
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Max. Sustained Turn = 11.3 deg/s
+100
0
-100
-300
+200
9G8G7G6G5G4G3G2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Quickest Turn = 20.8 deg/s
MA
XIM
UM
AIR
SP
EE
D
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
-200
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 23
+300
Quickest Turn = 17.3 deg/s
Maximum
allowed
AoA (28)
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
+100
0
-100
-200
-300
+200
9G8G7G6G5G4G3G2G
Turn Performance – 5,000 ft
Quickest Turn = 19.1 deg/s
Max. Sustained Turn = 10.2 deg/s
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 24
+300
Quickest Turn = 16 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 25
+100
0
-100
-200
-300
+300
9G8G7G6G5G4G3G2G
Quickest Turn = 15.1 deg/s
Max. Sustained Turn = 9.4 deg/s
Quickest Turn = 17.5 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
+200
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 26
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 12.8 deg/s
Max. Sustained Turn = 8.6 deg/s
+200
+300
Quickest Turn = 15.9 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 27
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 13.7 deg/s
Max. Sustained Turn = 7.2 deg/s
+200
Quickest Turn = 12.0 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 28
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 12.30 deg/s
Max. Sustained Turn = 6.1 deg/s
+200
Quickest Turn = 11.1 deg/s
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 29
+100
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 11.2 deg/s
Max. Sustained Turn = 5.1 deg/s
+200
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 10.5 deg/s
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 30
0
-100
-200
-300
9G8G7G6G5G4G3G2G
Quickest Turn = 9.0 deg/s
Max. Sustained Turn = 4.4 deg/s
+100
Maximum
allowed
AoA (28)
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 9.6 deg/s
Climb Performance
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 31
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•50% internal fuel
•GW= 16,194 lbs / 7,336 kg
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 32
0
50
100
150
200
250
300
350
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I - 1 - 33
0
50
100
150
200
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Acceleration Performances
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 34
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•50% internal fuel
•GW= 16,194 lbs / 7,336 kg
0
15
30
45
60
75
90
105
120
135
150
165
180
0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
30,000 30,000 36,000
0
15
30
45
60
75
90
105
120
135
150
165
180
0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
0 10,000 20,000
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : MIG-21M iz.96A
Engine :Tumanskiy R-11F2SK-200
CONFIGURATIONS :
•DRAG INDEX = 13 (4xR-3S)
•GW= 16,194 lbs / 7,336 kg
Sea Level
30,000 ft
36,000 ft30,000 ft
A1-Mikoyan-Gourevitch MIG-21M iz.96A-NFM-000-r6
I – 1 - 35
20,000 ft
10,000 ft
