dassault aviation mirage 2000 in falcon 4.0 rv &...
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Mirage 2000’s Flight Models by J.M. LANGERONV.5
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DASSAULT AVIATION Mirage 2000 in Falcon 4.0 RV & OF
WARNING: Information included in this document are not related to any “Real Life” planes, but only to the flight model (FM) built to be used in the Falcon 4.0 simulator. This flight model has been built only from public data, it does not refer to any classified nor confidential information.
Mirage 2000’s Flight Models by J.M. LANGERONV.5
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General Description.
Basic data
- Dry weight (-D, -N) : 7,900 kg (17439 lbs)- Dry weight (-C, -5) : 7,500 kg (16556 lbs)- Internal Fuel Capacity : 3150 kg (6966 lbs)- External additional tanks CAPACITY (-D,-N,-5):
o 2 wing tanks RPL-542: 6975lbs (3160 kg)o 1 fuselage tank RPL-522: 2,156lbs (980KG)o 3 tanks (2xRPL542 + 1xRPL-522) : 91540lbs (4140 KG)o Asymmetric (1xRPL542 + 1xRPL-522) : 5,650lbs (2560 Kg)
- Fuel Type: F-34 / F-35 / F-40 /F-43 / F-44.- Maximum Take Off Weight : 38,500 lbs- Maximum Landing On Weight : 24,000 lbs- Max Mach Number : 2.2 (-B, -C, -5, -9), 1.45 (-D, -N) (36,000 ft)- Max Indicated Air speed : 750 Kts- Operational Ceil: 57,500 ft (FL500 without stratospheric equipment)- Unofficial maximum altitude reached: 720,000 ft- Approach speed: between 140Kts (min. weight) and 200Kts (max. weight)- Max. Load Factor:
o CAT-I +9 (Ultimate +11) / -3.2G, AoA 29deg (Ultimate +31);o CAT-III +5.5/-3.2G AoA 20deg
- Reference Area: 441 ft2 (40.5 m2)- Length :14.94 m- Wing Span : 9.13 m- Height (with weight less than 25,000 lbs) : 5.20 m- Maximum AoA for hard landing (rear contact) at weight of 21,800lbs :15°30’
Power Plant: 1 SNECMA M53-P2- Dry Thrust : 65 kN - AB Thrust:
o Nominal: 97kN (21,800 lbs)o Null Air Speed, FL0 : 75kN (16,900 lbs)o Mach 0.9, FL0 : 106kN (23,850 lbs)
- Specific fuel flow with full AB: 2,12 kg/DANH.H - Specific fuel flow with MIL power: 0.92 kg/DANH.H
Versions
The Mirage 2000 family contains the following version, available in F4: Mirage 2000-B Twin Seat French Air Force training version Mirage 2000-C (RDI) Single Seat AA for French Air Force Mirage 2000-N (N for Nuclear) Twin Seat French Air Force with Nuclear
capacity Mirage 2000-D (D for Diversified) Twin Seat AG for French Air Force. Mirage 2000-5(F) Single Seat AA for French Air Force Mirage 2000-5 Mk2 Export version of –5, Single or Twin Seat. Mirage 2000-9 Single of Twin Seat Export version
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Main differences are:
Mirage 2000-C and –5 are mainly AA, -C is limited to Fox-1 capacity when –5 has Fox-3 (MICA-EM and MICA-IR since end of 2006) with multiple target tracking. ECM of the –5 has been significantly improved versus –C
Mirage 2000-B is a twin seat version dedicated to training and pilot transformation, both seats are dedicated to pilots.
Mirage 2000-D and –N, are twin seat, one pilot, one Weapon System Officer (WSO, called NOSA in French), they do not have internal DEFA gun, nor air intake mobile devices, so, mach number is limited to 1.45. As they are mainly dedicated to AG, they host the Antilope-5 TC (Coherent Processing) radar, with few little AA capabilities.
Radar:
2000-C : RDI: AA mode, Single target tracking , Look down-Shoot down, high range (60 Nm / 360 656 ft for SER of 5 m2, over or under flight level) . Compatible with MATRA Super-530D (Fox1), No TFR nor TWS
2000-5 : RDY: AA mode, Multiple targets tracking , Look down-Shoot down, high range (70 Nm / 426 230 ft for SER of 5 m2, over or under flight level) . Compatible with MICA ER (Fox-3) with LAM allowing shoot of 2 MICA before missile lock, others in Mad-Dog or Pit-Bull mode, TWS capable, but no TFR
2000-9 : RDY-2: AA mode, Multiple targets tracking , Look down-Shoot down, high range (80 Nm / 491 803 ft for SER of 5 m2, over or under flight level) . Compatible with MICA ER (Fox-3) with LAM allowing shoot of 2 MICA before missile lock, others in Mad-Dog or Pit-Bull mode, TWS and TFR capable
2000-D : DASSAULT ELECTRONIQUE Antilope-5, mainly AG, allowing low altitude / high speed ground following (200 ft , 600Keas, +5.5G) with heavy loads (2 RPL-541/542 + 2 Magic-2 + 2 BGL-250 or 4 Mk82) but with few AA capability : AG range of 27Nm (163934 ft), AA range limited to 10 Nm in a mode close to F16’s ACM), no TWS, nor NTCR capabilities.
Electronic Counter Measures:
Radar cross section (RCS) is assume to be less than the F-16 one a 80% is reasonable.
ECM are internal (no Pods) and combine passive sensor, active jamming and chaff/ flare dispensers
- Maximum chaff number set to 112 for all French 2000 variants- Maximum flare number set to 64 for all French 2000 variants- 2000-D has additional dorsal equipment allowing 48 more flare or chaff
(160 / 64 or 112 / 112)
ECM Systems includes- Thomson-CSF Serval radar warning receiver (antennae at each wingtip and on
trailing-edge of fin, near tip, plus VCM-65 cockpit display); - Thomson-CSF Caméléon (2000N), Caméléon C2 (2000D) or Sabre (2000C) jammer
at base of fin (detector on fin leading-edge); - Matra Bae Spirale, comprising chaff dispensers in Karman fairings at wing
trailing-edge/fuselage intersection and flares in lower rear fuselage.
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- French Air Force DDM (Détecteur Départ Missile) missile plume detector requirement satisfied by 1994 purchase of SAGEM SAMIR system for 1995 fitment in rear of Magic launch rails (2000D/N first, but also to 2000Cs patrolling Bosnia).
- Spirale fitted to 2000N-K2; retrofitted to 2000N-K1 and installed on 2000Cs from No. 93;
- Thomson-CSF Eclair system (Alkan LL5062 chaff and flare launcher) in place of braking parachute, lacking automatic operation on 2000C before Rank 93, can be installed on 2000-D and N if necessary
Weapon Loads
M2000-D Loads by Hard Points
Load 8 6 4 2 1 3 5 7 9Max weight (kg) 300 1800 400 400 1800 400 400 1800 300R 5 5 0 Magic-II 1 1RPL-541 /RPL-542
(2000L)1 1
RPL-501/ RPL-502(1700L)
1 1
RPL-522(1300L Supersonic)
1
Mk-82 / BSU-49 4 1 1 4 1 1 4BGL-1000 / GBU-24 1 1 1BGL-250 / GBU-12 2 2 2BLU-107 DURANDAL 1 1 4 1 1BAP-100 / BAT-120 18BLG-66 BELOUGA 1 1 1 1 1 1 1Targeting Pod 1
AS-30L(*) 1 1APACHE 1
ARMAT AS-37 1 1EXOCET AM-39 1 1FLIR Pod 1SCALP-EG 1Recco Pod 1
2x DEFA 30mm 1Refueling Pod 1
1 98 6 724
35
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M2000-C loads by Hard Points :
As Mirage 2000-C we mean French Air Force aircraft –C RDI with Fox-1 capacity by Matra Super-530D missile.Internal loads are 2 DEFA-554 30mm guns with firing rate of 1500/1800 round per minutes each (30 per sec), so with 125 rounds per gun, firing time is about 4 to 5 seconds.
Load 8 6 4 2 1 3 5 7 9Max weight (kg) 300 1800 400 400 1800 400 400 1800 300R 5 5 0 Magic-II 1 1
Super 530D 1 1RPL-541 /RPL-542
(2000L) 1 1
RPL-501/ RPL-502(1700L)
1 1
RPL-522(1300L Supersonic)
1
Mk-82 / BSU-49 4 1 1 4 1 1 4
M2000-5 loads by Hard Points :
Load 8 6 4 2 1 3 5 7 9Max weight (kg) 300 1800 400 400 1800 400 400 1800 300R 5 5 0 Magic-II 1 1
Mica EM 1 1 1 1RPL-541 /RPL-542
(2000L)1 1
RPL-501/ RPL-502(1700L)
1 1
RPL-522(1300L Supersonic)
1
Mk-82 / BSU-49 4 1 1 4 1 1 4
Drag Index of Standard Weapons1 - Drag Index Values are those read in Falcon 4.0 “Ammunition panel”, and are not to be compared with real-life Drag Index values using “DASSAULT AVIATION” nor “Armée de l’Air” convention.2 – Drag index values are here to be understood including the related pylon.
MATRA R550 Magic-II (with its pylon) : +7 MICA (EM or IR) (with its pylon) : +8 MATRA Super 530D (with its pylon) : +8 RPL-541/542 : +30 RPL-522 : +30 AS-30 L (with its pylon) : +8 2 x GBU-12 (GP) : +37
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Standard Configurations
Mirage 2000-C
Configuration Name : Fox = 1xRPL-522 + 2xSuper-530D + 2xMagic-IIConfiguration Name : Bravo = 2xRPL-541/542 + 2xMagic-IIConfiguration Name : Kilo = 1xRPL-522 + 2xRPL-541/542 + 2xMagic-II
Mirage 2000-5
Configuration Name : Fox = 1xRPL-522 + 4xMICA-EM + 2xMagic-IIConfiguration Name : Bravo = 2xRPL-541/542 + 4xMICA-EM + 2xMagic-IIConfiguration Name : Kilo = 1xRPL-522 + 2xRPL-541/542 + 4xMICA-EM + 2xMagic-II
Mirage 2000-D
Loads : 2xRPL-541/542 + 2xMagic-II, 3,300lbs internal fuel:With flaps and gear down, minimum speed: 115Kts (CAS)Rotation speed (Take-Off) 145KtsApproach speed 155Kts with AoA of 12-14 deg (1,500lbs fuel remaining)Flaps and Gear up, 80% RPM give 350Kts (CAS) at sea level.VNE (Velocity Never Exceed) : 600 Kts / M=0.98 (Ultimate M=1.05)
All configurations involving RPL-541/542 are limited to M=0.98 (ultimate M=1.05), RPL-522 seems to be limited to M=1.6
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Roll Rate Set of curves giving Maximum roll rate (deg/sec) and time to roll 90deg at constant speed versus Angle of Attack
Peak Roll rate function of Angle of attack (for a given Dynamic pressure in QBar), Clean configuration, 50% internal fuel
0
50
100
150
200
250
300
-10 0 10 20 30
AoA (deg)
Ro
ll R
ate
(d
eg/s
)
200
400
600
800
2000
Fuel Flow.
Fuel flow (Real Life Data, not F4)Configuration: Mirage 2000-C, Full AB
FL0, M=0.5 : 47,500 lbs/h (360 Kg/min) FL150, M=0.8 : 36,500 lbs/h (275 Kg/min) FL360, M=1.4 : 30,500 lbs/h (230 Kg/min)
Configuration: Mirage 2000-D, 2x2000L + 2xBGL-250 + 2xMagic, 100% internal Fuel Taxiway : 2,400 lbs/h (23 l/min, 18 Kg/min) FL400, M=0.8 : 3,950 lbs/h (38 l/min, 30 Kg/min) FL0, 450 Kts (RPM=86%) : 9,500 lbs/h (90 l/min, 72 Kg/min)
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Level Flight EnvelopeMirage 2000-C
Mirage 2000-5F
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Full AB
0
10,000
20,000
30,000
40,000
50,000
60,000
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
Alt
(ft
)
GW=9t Clean
GW=9.4t + 2 Magic
GW=10.0t + 2 Magic + 4 MICA
GW=10.5t + 2 Magic + 4 MICA + RPL522
VNE
Ma
xim
um a
llow
ed
mac
h n
umbe
r
0
10,000
20,000
30,000
40,000
50,000
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 1.50Mach
Alt
(ft
)
GW=9.0t Clean
GW=9.4t+ 2 Magic
GW=8.7t + 2 Magic + RPL522
GW=15.3t + 2 RPL541/542 + 2 GBU-12
Level Flight Envelope
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•MILL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
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Level Flight EnvelopeMirage 2000-DMirage 2000-N
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0
10,000
20,000
30,000
40,000
50,000
60,000
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60
Mach
Alt
(ft
)
GW=9.4tDI=14 / 2-R550
GW=9.0tDI=0
GW=11.3tDI=60 / RPL-541/542
GW=15.7tRPL-541/542 & 2GBU-12
0
10,000
20,000
30,000
40,000
50,000
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
Mach
Alt
(ft
)
GW=9.4tDI=14 / 2-R550
GW=9.0tDI=0
GW=11.3tDI=60 / RPL-541/542
GW=15.7tRPL-541/542 & 2GBU-12
Level Flight Envelope
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•MILL Power
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
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Turn PerformanceAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
Maximum Sustained Turn Rate
0.00
5.00
10.00
15.00
20.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00
mach number
Su
sta
ine
d t
urn
ra
te d
eg
/s
0
10,000
15,000
20,000
35,000
Maximum Available Turn Rate
0.00
5.00
10.00
15.00
20.00
25.00
30.00
0.00 0.50 1.00 1.50 2.00
Mach number
Ma
xim
um
ins
tan
tan
eou
s t
urn
rat
e (
deg
/s)
0
10,000
15,000
20,000
30,000
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Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
Maximum Sustained Load Factor (Ng)
0.00
2.00
4.00
6.00
8.00
10.00
150 200 250 300 350 400 450 500 550 600 650 700 750
CAS (Kts)
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
0
10,000
15,000
20,000
35,000
Maximum Available Load Factor
0.00
2.00
4.00
6.00
8.00
10.00
0.00 0.50 1.00 1.50 2.00
Mach number
Ma
xim
um
Av
ail
ab
le L
oa
d F
acto
r (N
g)
0
10,000
15,000
20,000
30,000
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0.00
4.00
8.00
12.00
16.00
20.00
24.00
28.00
32.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-250
-500
-1000
+400
+600
9G8G
7G
6G
5G
4G
3G
2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
Quickest Turn = 27.36 deg/s
Max. Sustained Turn = 16.13 deg/s
MA
XIM
UM
AIR
SP
EE
D
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0.00
4.00
8.00
12.00
16.00
20.00
24.00
28.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-250
-500
-1000
+400
+600
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW = 10.6t / 23,500 lbs
Quickest Turn = 25.06 deg/s
Max. Sustained Turn = 14.37 deg/s
MA
XIM
UM
AIR
SP
EE
D
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0.00
4.00
8.00
12.00
16.00
20.00
24.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
-500
-1000
+200
0
-250
+400
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 23.20 deg/s
Max. Sustained Turn = 12. 73 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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0.00
4.00
8.00
12.00
16.00
20.00
24.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-400
-800
-1600
+400
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 21.37 deg/s
Max. Sustained Turn = 11.22 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-400
-800
-1600
+400
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 19.62 deg/s
Max. Sustained Turn = 9.80 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-400
-800
-1600
+400
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 17.76 deg/s
Max. Sustained Turn = 8.59 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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0.00
4.00
8.00
12.00
16.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-500
-1000
-2000
+400
9G8G
7G
6G
5G
4G
3G
2G
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 14.52 deg/s
Max. Sustained Turn = 7.48 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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0.00
4.00
8.00
12.00
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 Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-500
-1000
-2000
+400
9G8G7G6G
5G
4G
3G
2G
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 11.73 deg/s
Max. Sustained Turn = 6.07 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t
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Turn PerformanceAircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
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Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Maximum Available Turn Rate
0.00
5.00
10.00
15.00
20.00
0.00 0.50 1.00 1.50 2.00
Mach number
Ma
xim
um
ins
tan
tan
eou
s t
urn
rat
e (
deg
/s)
0
10,000
15,000
20,000
30,000
Maximum Sustained Turn Rate
0.00
5.00
10.00
15.00
20.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00
mach number
Su
sta
ine
d t
urn
ra
te d
eg
/s
0
10,000
15,000
20,000
35,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 25 / 71
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Maximum Available Load Factor
0.00
1.00
2.00
3.00
4.00
5.00
6.00
0.00 0.50 1.00 1.50 2.00
Mach number
Ma
xim
um
Av
ail
ab
le L
oa
d F
acto
r (N
g)
0
10,000
15,000
20,000
30,000
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Maximum Sustained Load Factor (Ng)
0.00
1.00
2.00
3.00
4.00
5.00
6.00
150 200 250 300 350 400 450 500 550 600 650 700 750
CAS (Kts)
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
0
10,000
15,000
20,000
35,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 26 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
) Max. Sustained Turn = 12.79 deg/s
+200
0
-250
-500
+400
9G8G7G
6G
5G
4G
3G
2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 17.46 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 27 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)
Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 11.45 deg/s
+200
0
-250
-500
+400
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 16.06 deg/s
MA
XIM
UM
AIR
SP
EE
D
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 28 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 10.21 deg/s
+200
0
-250
-500
+400
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 14.80 deg/s
MA
XIM
UM
AIR
SP
EE
D
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 29 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 8.95 deg/s
+200
0
-250
-500
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 13.67 deg/s
MA
XIM
UM
AIR
SP
EE
D
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 30 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 7.78 deg/s
+200
0
-250
-500
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 12.49 deg/s
MA
XIM
UM
AIR
SP
EE
D
-1000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 31 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 6.86 deg/s
+200
0
-250
-500
9G8G7G
6G
5G
4G
3G
2GQuickest Turn = 11.41 deg/s
MA
XIM
UM
AIR
SP
EE
D
-1000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 32 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 5.94 deg/s
+200
0
-250
-500
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 9.71 deg/s
MA
XIM
UM
AIR
SP
EE
D
-1000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 33 / 71
0.00
4.00
8.00
12.00
16.00
20.00
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
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)
Max. Sustained Turn = 4.79 deg/s
+200
0
-250
-500
9G8G7G
6G
5G
4G
3G
2G
Quickest Turn = 7.77 deg/s
-1000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 34 / 71
Turn PerformanceAircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 35 / 71
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)Maximum available Turn Rate
0.00
5.00
10.00
15.00
20.00
0.00 0.50 1.00
Mach number
Ma
xim
um
inst
an
tan
eo
us
turn
rat
e (
deg
/s)
0
10,000
15,000
20,000
30,000
Sustained Turn Rate
0.00
5.00
10.00
15.00
20.00
0.000 0.100 0.200 0.300 0.400 0.500 0.600 0.700 0.800 0.900 1.000
mach number
Su
sta
ine
d t
urn
ra
te d
eg
/s 0
10,000
15,000
20,000
35,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 36 / 71
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)Maximum Available Load Factor
0.00
1.00
2.00
3.00
4.00
5.00
6.00
0.00 0.20 0.40 0.60 0.80 1.00
Mach number
Lo
ad
Fa
cto
r (N
g) 0
10,000
15,000
20,000
30,000
Sustained G
0.00
1.00
2.00
3.00
4.00
5.00
6.00
150 200 250 300 350 400 450 500 550 600 650 700 750
CAS (Kts)
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
0
10,000
15,000
20,000
35,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 37 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
+200
0
-250
-500
+400
9G8G7G6G5G
4G
3G
2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 17.52 deg/s
Max. Sustained Turn = 13.07 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 38 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
+400
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 16.23 deg/s
Max. Sustained Turn = 11.70 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 39 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
+400
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 14.93 deg/s
Max. Sustained Turn = 10.41 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 40 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(d
eg
ree
pe
r se
con
d)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 13.77 deg/s
Max. Sustained Turn = 9.14 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 41 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 12.66 deg/s
Max. Sustained Turn = 7.95 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 42 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
9G8G7G6G5G
4G
3G
2GQuickest Turn = 11.55 deg/s
Max. Sustained Turn = 7.00 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 43 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 9.91 deg/s
Max. Sustained Turn = 6.08 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 44 / 71
0.00
4.00
8.00
12.00
16.00
20.00
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t•CdVE “Charges” (+5.5G – AoA < 20)
+200
0
-250
-500
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 7.94 deg/s
Max. Sustained Turn = 4.90 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.9
5)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 45 / 71
Climb Performance
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 46 / 71
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 14•GW=20,500lbs / 9.3 t
0
10,000
20,000
30,000
40,000
50,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
x C
lim
b R
ate
(ft
/min
)
0.00
0.20
0.40
0.60
0.80
1.00
1.20
1.40
1.60
1.80
2.00
2.20
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
ch n
um
ber
giv
ing
Max
Clim
b R
ate
Mach number given best Climb Rate
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 47 / 71
0
100
200
300
400
500
600
700
800
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
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 14•GW=20,500lbs / 9.3 t
Climb Angle
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 48 / 71
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 14•GW=20,500lbs / 9.3 t
Mach number given best Climb Rate
0
10,000
20,000
30,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
x C
lim
b R
ate
(ft
/min
)
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
ch n
um
ber
giv
ing
Max
Clim
b R
ate
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 49 / 71
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
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
0
100
200
300
400
500
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
Mach
Exc
ess
Sp
ecif
ic P
ow
er
(ft/
s) 0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 14•GW=20,500lbs / 9.3 t
Climb Angle
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 50 / 71
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)•GW=20,500lbs / 10.5 t
0
10,000
20,000
30,000
40,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
x C
limb
Ra
te (
ft/m
in)
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Mac
h n
um
ber
giv
ing
Ma
x C
limb
Ra
te
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 51 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)•GW=20,500lbs / 10.5 t
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
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
0
100
200
300
400
500
600
700
800
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
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Climb Angle
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 52 / 71
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)•GW=20,500lbs / 10.5 t
0
10,000
20,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Max
Cli
mb
Rat
e (
ft/m
in)
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Mac
h n
um
ber
giv
ing
Max
Clim
b R
ate
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 53 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)•GW=20,500lbs / 10.5 t
Climb Angle
0
100
200
300
400
500
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
Mach
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 54 / 71
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
ch n
um
be
r g
ivin
g M
ax
Clim
b R
ate
0
10,000
20,000
30,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Max
Clim
b R
ate
(ft/
min
)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 55 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Climb Angle
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
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
Mach
Cli
mb
An
gle
(d
eg)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
0
100
200
300
400
500
600
700
800
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
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 56 / 71
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
0
10,000
20,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Max
Clim
b R
ate
(ft/
min
)
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Ma
ch n
um
ber
giv
ing
Max
Clim
b R
ate
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 57 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Climb Angle
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
0
100
200
300
400
500
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
Mach
Exc
ess
Sp
ecif
ic P
ow
er
(ft/
s) 0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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
Mach
Cli
mb
An
gle
(d
eg)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 58 / 71
0
5,000
10,000
15,000
20,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Max
Clim
b R
ate
(ft
/min
)
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Mac
h n
um
be
r g
ivin
g M
ax
Cli
mb
Rat
e
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 59 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
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
Mach
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Climb Angle
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 60 / 71
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
0
5,000
10,000
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Max
Clim
b R
ate
(ft
/min
)
0.00
0.20
0.40
0.60
0.80
1.00
0 10,000 20,000 30,000 40,000 50,000 60,000
Altitude (ft)
Mac
h n
um
be
r g
ivin
g M
ax
Cli
mb
Rat
e
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 61 / 71
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
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
Mach
Exc
ess
Sp
eci
fic
Po
wer
(ft
/s)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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
Mach
Cli
mb
An
gle
(d
eg)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Climb Angle
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 62 / 71
Acceleration & Deceleration
Performances
Mirage 2000-CMirage 2000-5F
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 63 / 71
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 14•GW=20,500lbs / 9.3 t
0
20
40
60
80
100
0.50 1.00 1.50 2.00
Mach
Tim
e (
s)
0
10,000
20,000
0
30
60
90
120
150
180
0.50 1.00 1.50 2.00 2.50
Mach
Tim
e (
s)
30,000
36,000
45,000
RL 36,000ft
Sea Level
10,000 ft20,000 ft
30,000 ft
45,000 ft
36,000 ft
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 64 / 71
Deccelration Diagram - Throttle set to Idle
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Idle
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
Conf A : GW = 20,500lbs/9.4t 2xR550Conf B :GW = 26,600lbs/12t 2xRPL541/542 + 2xR550 + 4xMICA
Conf C : Conf A + Air Brakes
0
30
60
90
120
150
0.30 0.50 0.70 0.90 1.10 1.30 1.50 1.70
Mach
Tim
e (s
eco
nd
s)
A-5,0
00ft
B-5,000ft
C-5,000ft
A-15,000ft
B-15,000ft C-15,000ft B-25,000ft
A-25,000ft
C-25,000ft
Conf A : GW = 20,500lbs/9.4t 2xR550Conf B :GW = 26,600lbs/12t 2xRPL541/542 + 2xR550 + 4xMICA
Conf C : Conf A + Air Brakes
0
30
60
90
120
150
180
210
0.70 0.90 1.10 1.30 1.50 1.70
Mach
Tim
e (s
eco
nd
s)
A-35,000ft
B-35,000ft C-35,000ft
A-45,000ft
B-45,000ft
C-45,000ft
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 65 / 71
Fuel flowEndurance and
Autonomy
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 66 / 71
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
Fuel Flow for Sustained Mach number
0
5,000
10,000
15,000
20,000
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Flo
w (
lbs
/ h)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Best Mach number for Endurance and Autonomy
0
10,000
20,000
30,000
40,000
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Alt
itu
de
Best Autonomy(dist. / lbs)
Best Endurance(time / lbs)
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 67 / 71
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-CEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)•GW=28,000lbs / 12.7 t
Endurance for Sustained Mach number
0.00
5.00
10.00
15.00
20.00
25.00
30.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Tim
e (m
in)
for
1,00
0 lb
s K
RO 0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Autonomy for Sustained Mach number
0.00
20.00
40.00
60.00
80.00
100.00
120.00
140.00
160.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Dis
tan
ce
(Nm
) fo
r 1
,00
0 lb
s K
RO
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 68 / 71
Best Mach number for Endurance and Autonomy
0
10,000
20,000
30,000
40,000
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90
Mach
Alt
itu
de
Best Autonomy(dist. / lbs)
Best Endurance(time / lbs)
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 106 •2xR550 + 4xMICA + RPL-541/542•GW=26,600lbs / 12.0 t
Fuel Flow for Sustained Mach number
0
5,000
10,000
15,000
20,000
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Flo
w (
lbs
/ h)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 69 / 71
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-5FEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 106 •2xR550 + 4xMICA + RPL-541/542•GW=26,600lbs / 12.0 t
Endurance for Sustained Mach number
0.00
5.00
10.00
15.00
20.00
25.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Tim
e (m
in)
for
1,00
0 lb
s K
RO 0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Autonomy for Sustained Mach number
0.00
20.00
40.00
60.00
80.00
100.00
120.00
140.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Dis
tan
ce
(Nm
) fo
r 1
,00
0 lb
s K
RO
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 70 / 71
Best Mach number for Endurance and Autonomy
0
10,000
20,000
30,000
40,000
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90
Mach
Alt
itu
de
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
Best Autonomy(dist. / lbs)
Best Endurance(time / lbs)
Fuel Flow for Sustained Mach number
0
5,000
10,000
15,000
20,000
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Flo
w (
lbs
/ h)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Mirage 2000’s Flight Models by J.M. LANGERONV.5
Page 71 / 71
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Mirage 2000-DEngine :SNECMA M53-P2
CONFIGURATIONS :•DRAG INDEX = 111 2xR550 - 2xGBU-12- 2xRPL-541/542•GW=33,750lbs / 15.7 t
Endurance for Sustained Mach number
0.00
5.00
10.00
15.00
20.00
25.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Tim
e (m
in)
for
1,00
0 lb
s K
RO 0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Autonomy for Sustained Mach number
0.00
20.00
40.00
60.00
80.00
100.00
120.00
140.00
0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00
Mach
Dis
tan
ce
(Nm
) fo
r 1
,00
0 lb
s K
RO
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000