Natops Flight Manual Mig 21m
January 20, 2017 | Author: Atamvir Singh Multani | Category: N/A
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Download Natops Flight Manual Mig 21m...
Description
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
PERFORMANCE ANALYSIS
Mig-21 M / L-15 Mikoyan-Gourevitch Corporation (Tumanskiy R-11F2SK-200) DOCUMENT Reference : A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-rev.1 / Wednesday, December 23, 2009 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 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/)
I–1-1
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Level Flight Envelope
I–1-2
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Level Flight Envelope DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •Max AB
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200 Level Flight Enveloppe Full AB
65,000
2 x K-13 GW = 15,258 lbs
60,000 55,000 50,000 45,000
2 x K-13 GW = 17,731lbs
35,000 30,000 25,000
20,000
650 Kts (IAS)
15,000 10,000 5,000
0 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
Mach
DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •MILL Power
AA1
Clean
AA4
Aircraft : VNE Mig-21 M AA4 Engine :Tumanskiy R-11F2SK-200
Level Flight Enveloppe MIL Power
65,000 60,000
55,000
2 x K-13 GW = 15,258 lbs
50,000 45,000 40,000
Alt (ft)
Alt (ft)
40,000
35,000 30,000 25,000 20,000 15,000 10,000
650 Kts (IAS)
2 x K-13 GW = 17,731 lbs
5,000 0 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 Mach AA1 AA2
I–1-3
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200 CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •50% internal fuel •GW= 15,589 lbs / 7,062 kg
I–1-4
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Rate – Summary DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg Maximum Available Turn Rate
25.00 0 10,000 20,000 30,000
Maximum instantaneous turn rate (deg/s)
20.00
40,000
Max Turn reached without AoA limit (Stall speed) Ng < 7 in subsonic, Ng < 6 in supersonic
15.00
10.00
5.00
0.00 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
Mach number
Maximum Sustained Turn rate (deg/s) 25.00 0 10,000 20,000 30,000
Sustained Turn rate (deg/s)
20.00
40,000
15.00
10.00
5.00
0.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
Mach number
I-1-5
1.40
1.60
1.80
2.00
2.20
2.40
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Load Factor – Summary DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg Maximum Available Load Factor
8.00
0 10,000 20,000
7.00
40,000
6.00
5.00
4.00
Max Turn reached without AoA limit (Stall speed) Ng < 7 in subsonic, Ng < 6 in supersonic
3.00
2.00
1.00 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
Mach number
8.00
0 10,000
7.00
20,000 30,000
6.00
Sustained Load Factor (Ng)
Maximum Available Load Factor (Ng)
30,000
40,000
5.00
4.00
3.00
2.00
1.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
Mach number
I-1-6
1.40
1.60
1.80
2.00
2.20
2.40
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – Sea Level DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G
3G
4G
5G
6G
7G
8G
9G
22.00
Quickest Turn = 21.3 deg/s 20.00
Quickest Turn = 19.36 deg/s 18.00
-300 -200 14.00
-100
12.00
0
10.00
Maximum allowed AoA (33)
Max. Sustained Turn = 11.64 deg/s
+100
MAXIMUM AIR SPEED
Turn Rate (degree per second)
16.00
8.00
+200 6.00
4.00
+300
2.00
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I–1-7
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 5,000 ft
24.00
DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
2G
3G
4G
5G
6G
7G
8G
9G
22.00
20.00
Quickest Turn = 19.62 deg/s Quickest Turn = 17.94 deg/s
18.00
-300 -200 14.00
-100 12.00
Max. Sustained Turn = 10.77 deg/s 0
Maximum allowed AoA (33)
10.00
+100
MAXIMUM AIR SPEED
Turn Rate (degree per second)
16.00
8.00
+200 6.00
+300
4.00
2.00
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I–1-8
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 10,000 ft
24.00
DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
2G
3G
4G
5G
6G
7G
8G
9G
22.00
20.00
Quickest Turn = 18.72 deg/s 18.00
Quickest Turn = 16.73 deg/s
-300
14.00
-200 12.00
-100
Max. Sustained Turn = 9.92 deg/s
10.00
0
Maximum allowed AoA (33)
8.00
MAXIMUM AIR SPEED
Turn Rate (degree per second)
16.00
+100
6.00
4.00
+200 2.00
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I–1-9
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 15,000 ft DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G
3G 4G
5G
6G 7G
8G
9G
22.00
20.00
18.00
Quickest Turn = 16.33 deg/s
Turn Rate (degree per second)
16.00
Quickest Turn = 15.60 deg/s
Maximum allowed AoA (33)
14.00
-300 12.00
-200 -100
10.00
Max. Sustained Turn = 9.03 deg/s 0
8.00
MAXIMUM AIR SPEED
+100 6.00
+200 4.00
+300 2.00
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I – 1 - 10
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 20,000 ft DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G
3G 4G 5G 6G 7G 8G
9G
22.00
20.00
18.00
Turn Rate (degree per second)
16.00
Quickest Turn = 14.85 deg/s 14.00
Quickest Turn = 13.50 deg/s
Maximum allowed AoA (33)
12.00
-300 -200
10.00
-100 Max. Sustained Turn = 7.67 deg/s
8.00
0 MAXIMUM AIR SPEED
6.00
+100
+200
4.00
2.00
+300 0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I – 1 - 11
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 25,000 ft DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G
3G 4G 5G 6G 7G 8G
9G
22.00
20.00
18.00
Turn Rate (degree per second)
16.00
14.00
Quickest Turn = 12.53 deg/s Quickest Turn = 12.28 deg/s
Maximum allowed AoA (33)
12.00
10.00
-300 -200
8.00
-100 Max. Sustained Turn = 6.53 deg/s MAXIMUM AIR SPEED
0
6.00
+100 4.00
+200 2.00
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I – 1 - 12
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 30,000 ft DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G
3G 4G 5G 6G 7G 8G 9G
22.00
20.00
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 11.82 deg/s
Maximum allowed AoA (33)
10.00
-300 8.00
-200 -100
6.00
MAXIMUM AIR SPEED
Max. Sustained Turn = 5.41 deg/s 0
4.00
+100
2.00
+200
0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I – 1 - 13
450
500
550
600
650
700
750
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – 35,000 ft DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
24.00
2G 3G 4G 5G 6G 7G 8G
9G
22.00
20.00
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 10.03 deg/s
10.00
Maximum allowed AoA (33)
8.00
-300 -200
6.00
-100 MAXIMUM AIR SPEED
Max. Sustained Turn = 4.69 deg/s 0
4.00
+100 2.00
+200 0.00 0
50
100
150
200
250
300
350
400
CAS (Kts)
I – 1 - 14
450
500
550
600
650
700
750
I – 1 - 15
t CAS Nz CAS Nz
=0s = 594 Kts =7 G = 521 Kts =7 G 0
t = 6s CAS = 483 Kts Ng = 7G
t = 25.0 s CAS = 439 Kts Nz = 7 G
t = 21.2 s CAS = 211 Kts Ng = 3.41G
t = 16.4 s CAS = 355 Kts Ng = 7G
t = 11.6 s CAS = 435 Kts Ng = 7G
t = 13.4 s CAS = 523 Kts Nz = 7 G CONDITIONS: •Standard Day •Max AB •AoA limited to 33° CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg
5000
t = 6.8 s CAS = 558 Kts Ng = 7G Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
-5000
t = 19.4 s CAS = 486 Kts Nz = 7 G
360 deg turn started from Mach 0.9 Fastest 360 turn DATA BASIS : ESTIMATED
0
5000
10000
2 shoot
1 shoot
AC2 Path
AC1 Path
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Turn Performance – Sea Level
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Climb Performance
I – 1 - 16
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg Instantaneous Climb Rate
400
300
Excess Specific Power (ft/s)
0 5,000 10,000 15,000 20,000
200
25,000 30,000 35,000
40,000 45,000
100
0 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
Mach Angle Climb
90.00
80.00
70.00 0
60.00
Climb Angle (deg)
5,000 10,000
50.00
15,000 20,000
25,000
40.00
30,000
35,000
30.00
40,000
20.00
10.00
0.00 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 Mach
I - 1 - 17
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
DATA BASIS : ESTIMATED
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200
CONDITIONS: •Standard Day •MIL Power
CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) •GW=15,589 lbs / 7,062 kg Instantaneous Climb Rate
200
Excess Specific Power (ft/s)
0 5,000 10,000 15,000 20,000
100
25,000 30,000 35,000
40,000 45,000
0 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 2.50 Mach
Climb Angle 90.00
80.00
70.00 0
60.00
Climb Angle (deg)
5,000 10,000
50.00
15,000 20,000
25,000
40.00
30,000
35,000
30.00
40,000
20.00
10.00
0.00 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 Mach
I - 1 - 18
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Acceleration Performances
I – 1 - 19
A1-Mikoyan-Gourevitch Mig-21 M-NFM-000-r3
Acceleration Diagram DATA BASIS : ESTIMATED
CONDITIONS: 0 •Standard Day 10,000 •Max AB
Aircraft : Mig-21 M Engine :Tumanskiy R-11F2SK-200 CONFIGURATIONS : •DRAG INDEX = 12 (2xK-13) Acceleration (Max A/B Thrust) ISA Conditions •GW=15,589 lbs / 7,062 kg
20,000
180 165 150 135
10,000 ft 120
Time (s)
105
20,000 ft 90 75 60 45
Sea Level
30 15 30,000
0
30,000
0.30
0.40
36,000
0.50
0.60
0.70
Acceleration (Max A/B Thrust) Conditions 0.80 ISA0.90 1.00 1.10 Mach
1.20
1.30
1.40
1.50
1.60
180 165 150 135
30,000 ft 120
30,000 ft
Time (s)
105
36,000 ft
90
75 60 45 30
15 0 0.30
0.40
0.50
0.60
0.70
0.80
0.90
1.00
1.10
1.20
1.30
Mach
I – 1 - 20
1.40
1.50
1.60
1.70
1.80
1.90
2.00
2.10
2.20
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