dassault aviation mirage 2000 in falcon 4.0 free falcon 5

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Mirage 2000’s Flight Models by J.M. LANGERON V.5 Page 1 / 82 DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5 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.

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Page 1: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 1 / 82

DASSAULT AVIATION Mirage 2000

in Falcon 4.0 Free Falcon 5

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: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 2 / 82

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: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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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Mirage 2000’s Flight Models by J.M. LANGERON

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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 9

Max weight (kg) 300 1800 400 400 1800 400 400 1800 300

R 5 5 0 Magic-II 1 1

RPL-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

BGL-1000 / GBU-24 1 1 1

BGL-250 / GBU-12 2 2 2

BLU-107 DURANDAL 1 1 4 1 1

BAP-100 / BAT-120 18

BLG-66 BELOUGA 1 1 1 1 1 1 1

Targeting Pod 1

AS-30L(*) 1 1

APACHE 1

ARMAT AS-37 1 1

EXOCET AM-39 1 1

FLIR Pod 1

SCALP-EG 1

Recco Pod 1

2x DEFA 30mm 1

Refueling Pod 1

1 9 8 6 7 2

4

3

5

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Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 9

Max weight (kg) 300 1800 400 400 1800 400 400 1800 300

R 5 5 0 Magic-II 1 1

Super 530D 1 1

RPL-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 9

Max weight (kg) 300 1800 400 400 1800 400 400 1800 300

R 5 5 0 Magic-II 1 1

Mica EM 1 1 1 1

RPL-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 Weapons 1 - 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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Mirage 2000’s Flight Models by J.M. LANGERON

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Standard Configurations

Mirage 2000-C

Configuration Name : Fox = 1xRPL-522 + 2xSuper-530D + 2xMagic-II

Configuration Name : Bravo = 2xRPL-541/542 + 2xMagic-II

Configuration Name : Kilo = 1xRPL-522 + 2xRPL-541/542 + 2xMagic-II

Mirage 2000-5

Configuration Name : Fox = 1xRPL-522 + 4xMICA-EM + 2xMagic-II

Configuration Name : Bravo = 2xRPL-541/542 + 4xMICA-EM + 2xMagic-II

Configuration 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) 145Kts

Approach 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: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

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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

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)

Peak Rool Rate (AoA,Qbar)

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

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Mirage 2000’s Flight Models by J.M. LANGERON

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Level Flight Envelope

Mirage 2000-C

Mirage 2000-5F

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Level Flight Enveloppe

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

allo

we

d m

ach

num

be

r

Level Flight Enveloppe

MIL Power

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 : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MILL Power

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

Page 10: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Level Flight Envelope

Mirage 2000-D

Mirage 2000-N

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Level Flight Enveloppe

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

Mach

Alt

(ft

)

GW=9t Clean GW=9.4t + 2 Magic GW=11.3t 2 RPL-541/542

GW=15.7t2 Magic + 2 RPL-541/542 + 2GBU12

GW=9.4t

DI=14 / 2-R550

GW=9.0t

DI=0

GW=11.3t

DI=60 / RPL-541/542

GW=15.7t

RPL-541/542 & 2GBU-12

Level Flight Enveloppe

MIL Power

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=9.0t Clean GW=11.3t 2 RPL-541/542

GW=8.7t + 2 Magic + RPL522 GW=15.7t2 Magic + 2 RPL-541/542 + 2GBU12

GW=9.4t

DI=14 / 2-R550

GW=9.0t

DI=0

GW=11.3t

DI=60 / RPL-541/542

GW=15.7t

RPL-541/542 & 2GBU-12

Level Flight Envelope

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :SNECMA M53-P2

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MILL Power

Aircraft : Mirage 2000-D

Engine :SNECMA M53-P2

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Turn PerformanceAircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

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Turn Rate – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

0.00

5.00

10.00

15.00

20.00

25.00

30.00

0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20

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

0.00

5.00

10.00

15.00

20.00

25.00

30.00

0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40 1.60 1.80 2.00 2.20

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

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Load Factor – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

0.00

2.00

4.00

6.00

8.00

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

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

0.00

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

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

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

Max. Sustained Turn = 18.22 deg/s

+200

0

-200

-600

+400

+600

9G8G

7G

6G

5G

4G

3G

2G

Turn Performance – Sea Level

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Quickest Turn = 29.55 deg/s

MA

XIM

UM

AIR

SP

EE

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

-400

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

+200

0

-200

-400

-600

+400

+600

9G

8G

7G

6G

5G

4G

3G

2G

Turn Performance – 5,000 ft

Quickest Turn = 27.16 deg/s

Max. Sustained Turn = 16.25 deg/s

MA

XIM

UM

AIR

SP

EE

D

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

-400

-600

+200

0

-200

+400

9G

8G

7G

6G

5G

4G

3G

2G

Turn Performance – 10,000 ft

Quickest Turn = 24.84 deg/s

Max. Sustained Turn = 14.46 deg/s

MA

XIM

UM

AIR

SP

EE

D

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

+600

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

+200

0

-200

-400

-600

+400

9G

8G

7G

6G

5G

4G

3G

2G

Turn Performance – 15,000 ft

Quickest Turn = 22.95 deg/s

Max. Sustained Turn = 12.75 deg/s

MA

XIM

UM

AIR

SP

EE

D

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

+600

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

+200

0

-400

-600

-200

+400

9G

8G

7G

6G

5G

4G

3G

2G

Turn Performance – 20,000 ft

Quickest Turn = 20.93 deg/s

Max. Sustained Turn = 11.14 deg/s

MA

XIM

UM

AIR

SP

EE

D

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

Page 20: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

Turn Performance – 25,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

+200

0

-400

-600

-200

+400

9G

8G

7G

6G

5G

4G

3G

2G

Quickest Turn = 19.13 deg/s

Max. Sustained Turn = 9.8 deg/s

MA

XIM

UM

AIR

SP

EE

D

Page 21: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

Turn Performance – 30,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

+200

0

-400

-600

-200

+400

9G

8G

7G

6G

5G

4G

3G

2G

Quickest Turn = 16.62 deg/s

Max. Sustained Turn = 8.56 deg/s

MA

XIM

UM

AIR

SP

EE

D

Page 22: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

26.00

28.00

30.00

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

Tu

rn R

ate

(d

eg

ree p

er

seco

nd

)

Mach Number

AoAMax

-600

-400

-200

0

200

400

600

Turn Performance – 35,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14 (2xR550)

•GW=20,600lbs / 9.3 t

+200

0

-400-600

-200

9G

8G

7G

6G

5G

4G

3G

2G

Quickest Turn = 13.43 deg/s

Max. Sustained Turn = 7.0 deg/s

MA

XIM

UM

AIR

SP

EE

D

Page 23: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Turn PerformanceAircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 24: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Turn Rate – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :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

rate

de

g/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

in

sta

nta

ne

ou

s t

urn

ra

te (

de

g/s

)

0

10,000

15,000

20,000

30,000

Page 25: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Load Factor – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :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

ac

tor

(Ng

)

0

10,000

15,000

20,000

30,000

Page 26: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

+200

0

-250

-500

-1000

+400

+600

9G

8G

7G

6G

5G

4G

3G

2G

Turn Performance – Sea Level

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :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

Page 27: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 27 / 82

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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

+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 2000-5F

Engine :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

Page 28: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 28 / 82

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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

-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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 29: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-1600

-800

-400

0

200

400

600

+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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 30: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-1600

-800

-400

0

200

400

600

+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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 31: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-1600

-800

-400

0

200

400

600

+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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 32: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-2000

-1000

-500

0

200

400

600

+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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 33: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 s

ec

on

d)

AoAMax

-2000

-1000

-500

0

200

400

600

+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

D

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 0

•GW=23,500lbs / 10.6 t

Page 34: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Turn PerformanceAircraft : Mirage 2000-C

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 60

•GW=28,000lbs / 12.7 t

•CdVE “Charges” (+5.5G – AoA < 20)

Page 35: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 35 / 82

Turn Rate – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

in

sta

nta

ne

ou

s t

urn

ra

te (

de

g/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

rate

de

g/s

0

10,000

15,000

20,000

35,000

Page 36: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 36 / 82

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

ac

tor

(Ng

)

0

10,000

15,000

20,000

30,000

Aircraft : Mirage 2000-C

Engine :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

Page 37: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

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

D

Aircraft : Mirage 2000-C

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)

•GW=28,000lbs / 12.7 t

•CdVE “Charges” (+5.5G – AoA < 20)

Page 38: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 5,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 39: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 39 / 82

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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 10,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 40: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 40 / 82

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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 15,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

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Mirage 2000’s Flight Models by J.M. LANGERON

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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 s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 20,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 42: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 25,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 43: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 2.00

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 30,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 44: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

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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 2.00

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 35,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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

Page 45: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Turn PerformanceAircraft : Mirage 2000-D

Engine :SNECMA M53-P2

CONFIGURATIONS :

•RPL 541/542

•GW=27,500lbs / 12.4 t

Page 46: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Turn Rate – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

in

sta

nta

ne

ou

s t

urn

ra

te (

de

g/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

rate

de

g/s 0

10,000

15,000

20,000

35,000

Page 47: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Load Factor – Summary

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

Page 48: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

+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

.95)

Aircraft : Mirage 2000-D

Engine :SNECMA M53-P2

CONFIGURATIONS :

•RPL 541/542

•GW=27,500lbs / 12.4 t

•CdVE “Charges” (+5.5G – AoA < 20)

Page 49: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 5,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

Page 50: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 10,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 15,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

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V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 20,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

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V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 25,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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 = 11.55 deg/s

Max. Sustained Turn = 7.00 deg/s

MA

XIM

UM

MA

CH

NU

MB

ER

(M 0

.95)

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V.5

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 30,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

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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

Mach Number

Tu

rn R

ate

(d

eg

ree

pe

r s

ec

on

d)

AoAMax

-1000

-500

-250

0

200

400

600

Turn Performance – 35,000 ft

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :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

.95)

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Climb Performance

Page 57: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Maximum Instantaneous Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14

•GW=20,500lbs / 9.3 t

Maximum 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)

Max

Clim

b R

ate

(ft

/min

)

Maximum Climb Rate

Drag Index : 0 / 50% Internal Fuel

Full AB

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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

Mach number given best Climb Rate

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Instantaneous Clim Rate

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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

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

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 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14

•GW=20,500lbs / 9.3 t

Climb Angle

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Maximum Instantaneous Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14

•GW=20,500lbs / 9.3 t

Mach number given best Climb Rate

Maximum Climb Rate

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

)

Maximum Climb Rate

Drag Index : 0 / 50% Internal Fuel

Full AB

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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

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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

Mach

Clim

b A

ng

le (

deg

)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Instantaneous Clim Rate

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

Excess S

pecif

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 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14

•GW=20,500lbs / 9.3 t

Climb Angle

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Maximum Instantaneous Climb Rate

Mach number given best Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :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)

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

Clim

b R

ate

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Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 62 / 82

Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)

•GW=20,500lbs / 10.5 t

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

Clim

b A

ng

le (

deg

)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Instantaneous Clim Rate

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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Climb Angle

Page 63: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Maximum Instantaneous Climb Rate

Mach number given best Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-5F

Engine :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 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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

Page 64: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 76 (2xR550+4xMICA+RPL-522)

•GW=20,500lbs / 10.5 t

Climb Angle

Instantaneous Clim Rate

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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

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

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 65: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 65 / 82

Maximum Instantaneous Climb Rate

Mach number given best Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-C

Engine :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)

Mac

h 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 66: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Climb Angle

Aircraft : Mirage 2000-C

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)

•GW=28,000lbs / 12.7 t

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

Clim

b A

ng

le (

deg

)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Instantaneous Climb Rate

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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Page 67: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Maximum Instantaneous Climb Rate

Mach number given best Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-C

Engine :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 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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

Page 68: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Climb Angle

Aircraft : Mirage 2000-C

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 60 (2xR550+2xS530+RPL-522)

•GW=28,000lbs / 12.7 t

Instantaneous Climb Rate

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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

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

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 69: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Maximum Climb Rate

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 C

lim

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-D

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 111

2xR550 - 2xGBU-12- 2xRPL-541/542

•GW=33,750lbs / 15.7 t

Maximum Climb Rate

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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

Page 70: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 70 / 82

Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-D

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 111

2xR550 - 2xGBU-12- 2xRPL-541/542

•GW=33,750lbs / 15.7 t

Instantaneous Clim 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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

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

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 71: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 71 / 82

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-D

Engine :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

Maximum Climb Rate

0

5,000

10,000

0 10,000 20,000 30,000 40,000 50,000 60,000

Altitude (ft)

Max C

lim

b R

ate

(ft

/min

)

Maximum Climb Rate

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)

Mach

nu

mb

er

giv

ing

Max C

lim

b R

ate

Page 72: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Climb Rate

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-D

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 111

2xR550 - 2xGBU-12- 2xRPL-541/542

•GW=33,750lbs / 15.7 tInstantaneous Clim 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

Excess S

pecif

ic P

ow

er

(ft/

s)

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

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

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 73: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 73 / 82

Acceleration &

Deceleration

Performances

Mirage 2000-C

Mirage 2000-5F

Page 74: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 74 / 82

Acceleration Diagram

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Max AB

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2

CONFIGURATIONS :

•DRAG INDEX = 14

•GW=20,500lbs / 9.3 t

Acceleration from M0.5, 07 and 0.9 (AB)

Di=0, GW=20,500 lbs

0

20

40

60

80

100

0.50 1.00 1.50 2.00

Mach

Tim

e (

s)

0

10,000

20,000

Acceleration from M0.9 (AB)

Di=0, GW=20,500 lbs

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 75: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

Page 75 / 82

Deccelration Diagram - Throttle set to Idle

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•Idle

Aircraft : Mirage 2000-5F

Engine :SNECMA M53-P2Deceleration

Mach(t) with Throttle set to Idle

Conf A : GW = 20,500lbs/9.4t 2xR550

Conf 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 (

seco

nd

s)

5,000 ft Conf. A

5,000 ft Conf. B

5,000 ft Conf. C

15,000 ft Conf. A

15,000 ft Conf. B

15,000 ft Conf. C

25,000 ft Conf. A

25,000 ft Conf. B

25,000 ft Conf. C

A-5,0

00ft

B-5,000ft

C-5,000ft

A-15,000ft

B-15,0

00ft C-15,000ft

B-25,0

00ft

A-25,000ft

C-25,000ft

Deceleration

Mach(t) with Throttle set to Idle

Conf A : GW = 20,500lbs/9.4t 2xR550

Conf 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 (

seco

nd

s) 35,000 ft Conf. A

35,000 ft Conf. B

35,000 ft Conf.C

45,000 ft Conf. A

45,000 ft Conf. B

45,000 ft Conf. C

A-35,000ft

B-35,000ft C-35,000ft

A-45,000ft

B-45,000ft

C-45,000ft

Page 76: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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Fuel flow

Endurance and

Autonomy

Page 77: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-C

Engine :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 Endurance

Best Autonomy

Best Autonomy

(dist. / lbs)

Best Endurance

(time / lbs)

Page 78: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-C

Engine :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 (

min

) fo

r 1,0

00 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 1,0

00 lb

s K

RO

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Page 79: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 Endurance

Best Autonomy

Best Autonomy

(dist. / lbs)

Best Endurance

(time / lbs)

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-5F

Engine :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

Page 80: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-5F

Engine :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 (

min

) fo

r 1,0

00 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 1,0

00 lb

s K

RO

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000

Page 81: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

Mirage 2000’s Flight Models by J.M. LANGERON

V.5

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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 Endurance

Best Autonomy

DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-D

Engine :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

Page 82: DASSAULT AVIATION Mirage 2000 in Falcon 4.0 Free Falcon 5

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V.5

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DATA BASIS : ESTIMATED

CONDITIONS:

•Standard Day

•MIL Power

Aircraft : Mirage 2000-D

Engine :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 (

min

) fo

r 1,0

00 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 1,0

00 lb

s K

RO

0

5,000

10,000

15,000

20,000

25,000

30,000

35,000

40,000