DASSAULT AVIATION Mirage 2000 in Falcon 4.0 RV & OF · Mirage 2000-B is a twin seat version dedicated to training and pilot transformation, both seats are dedicated to pilots

Mirage 2000’s Flight Models by J.M. LANGERONV.5

Page 1 / 71

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.


Page 2 / 71

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


Page 3 / 71

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.


Page 4 / 71

- 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


Page 5 / 71

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


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


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


Page 6 / 71

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


Page 7 / 71

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)


Page 8 / 71

Level Flight EnvelopeMirage 2000-C

Mirage 2000-5F


Page 9 / 71

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



Page 10 / 71

Level Flight EnvelopeMirage 2000-DMirage 2000-N


Page 11 / 71

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



Page 12 / 71

Turn PerformanceAircraft : Mirage 2000-5FEngine :SNECMA M53-P2

CONFIGURATIONS :•DRAG INDEX = 0•GW=23,500lbs / 10.6 t


Page 13 / 71

Turn Rate – Summary

DATA BASIS : ESTIMATED

CONDITIONS:•Standard Day•Max AB



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


Page 14 / 71

Load Factor – Summary





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


Page 15 / 71

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





Quickest Turn = 27.36 deg/s

Max. Sustained Turn = 16.13 deg/s

MA

XIM

UM

AIR

SP

EE

D


Page 16 / 71

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




CONFIGURATIONS :•DRAG INDEX = 0•GW = 10.6t / 23,500 lbs



MA

XIM

UM

AIR

SP

EE

D


Page 17 / 71

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





Max. Sustained Turn = 12. 73 deg/s

MA

XIM

UM

AIR

SP

EE

DAircraft : Mirage 2000-5FEngine :SNECMA M53-P2



Page 18 / 71

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






MA

XIM

UM

AIR

SP

EE




Page 19 / 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)

+200

0

-400

-800

-1600

+400

9G

8G

7G

6G

5G

4G

3G

2G






MA

XIM

UM

AIR

SP

EE




Page 20 / 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

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






MA

XIM

UM

AIR

SP

EE




Page 21 / 71

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






MA

XIM

UM

AIR

SP

EE




Page 22 / 71

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






MA

XIM

UM

AIR

SP

EE




Page 23 / 71

Turn PerformanceAircraft : Mirage 2000-CEngine :SNECMA M53-P2

CONFIGURATIONS :•DRAG INDEX = 60•GW=28,000lbs / 12.7 t•CdVE “Charges” (+5.5G – AoA < 20)


Page 24 / 71




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


Page 25 / 71




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



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


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





MA

XIM

UM

AIR

SP

EE

DAircraft : Mirage 2000-CEngine :SNECMA M53-P2



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

)







+200

0

-250

-500

+400

9G8G7G

6G

5G

4G

3G

2G


MA

XIM

UM

AIR

SP

EE

D


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)







+200

0

-250

-500

+400

9G8G7G

6G

5G

4G

3G

2G


MA

XIM

UM

AIR

SP

EE

D


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)







+200

0

-250

-500

9G8G7G

6G

5G

4G

3G

2G


MA

XIM

UM

AIR

SP

EE

D


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)







+200

0

-250

-500

9G8G7G

6G

5G

4G

3G

2G


MA

XIM

UM

AIR

SP

EE

D

-1000


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)







+200

0

-250

-500

9G8G7G

6G

5G

4G

3G

2GQuickest Turn = 11.41 deg/s

MA

XIM

UM

AIR

SP

EE

D

-1000


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)







+200

0

-250

-500

9G8G7G

6G

5G

4G

3G

2G


MA

XIM

UM

AIR

SP

EE

D

-1000


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)







+200

0

-250

-500

9G8G7G

6G

5G

4G

3G

2G


-1000


Page 34 / 71

Turn PerformanceAircraft : Mirage 2000-DEngine :SNECMA M53-P2

CONFIGURATIONS :•RPL 541/542•GW=27,500lbs / 12.4 t


Page 35 / 71





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


Page 36 / 71





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


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






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)


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)






+200

0

-250

-500

+400

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

+400

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

9G8G7G6G5G

4G

3G

2GQuickest Turn = 11.55 deg/s


MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

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)






+200

0

-250

-500

9G8G7G6G5G

4G

3G

2G



MA

XIM

UM

MA

CH

NU

MB

ER

(M 0.9

5)


Page 45 / 71

Climb Performance


Page 46 / 71

Maximum Instantaneous Climb Rate





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


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





Climb Angle


Page 48 / 71



CONDITIONS:•Standard Day•MIL Power




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


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





Climb Angle


Page 50 / 71






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


Page 51 / 71

Climb Rate





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


Page 52 / 71







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


Page 53 / 71

Climb Rate





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


Page 54 / 71






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

)


Page 55 / 71

Climb Rate



Climb Angle



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


Page 56 / 71







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


Page 57 / 71

Climb Rate



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

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


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

)






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


Page 59 / 71

Climb Rate





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


Page 60 / 71







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


Page 61 / 71

Climb Rate





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


Page 62 / 71

Acceleration & Deceleration

Performances

Mirage 2000-CMirage 2000-5F


Page 63 / 71

Acceleration Diagram





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


Page 64 / 71

Deccelration Diagram - Throttle set to Idle


CONDITIONS:•Standard Day•Idle


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


Page 65 / 71

Fuel flowEndurance and

Autonomy


Page 66 / 71





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)


Page 67 / 71





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


Page 68 / 71


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






CONFIGURATIONS :•DRAG INDEX = 106 •2xR550 + 4xMICA + RPL-541/542•GW=26,600lbs / 12.0 t


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


Page 69 / 71




CONFIGURATIONS :•DRAG INDEX = 106 •2xR550 + 4xMICA + RPL-541/542•GW=26,600lbs / 12.0 t


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


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


Page 70 / 71


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








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


Page 71 / 71






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


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

Documents

DASSAULT AVIATION Mirage 2000 in Falcon 4.0 RV & OF · Mirage 2000-B is a twin seat version dedicated to training and pilot transformation, both seats are dedicated to pilots