View
228
Download
7
Category
Preview:
Citation preview
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 1 / 55
DASSAULT AVIATION Rafale in Falcon 4.0. RedViper
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.
Special thanks to testers and reviewers:
- HighSpeed (C6)- Jojo (C6)- Mav-JP (C6)- JimG (FF)- Saint (FF)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 2 / 55
General Description.
Rafale is a light (10 tons) Omni-Role (AA and AG) fighter, twin engine (50 / 75kN each), with high-end weapon and navigation system (Multi target BVR, data link, Optronic sensors, Stand Off and Laser Guided AG weapons capabilities)
Its advanced aerodynamic configuration and full digital flight control system provide a very high level of maneuverability.
Its Speed range (750 Knots IAS , Mach 1.8) is more affordable (with supersonic capabilities without After Burner and/or with external tanks), than wide in itself (compared to Mach 2.2 of Mirage 2000-5 for example)
Versions
The airframe of the Rafale is declined as of today in 4 versions: Rafale C : single seat, Air Force Rafale B : two seats, Air Force Rafale M : single seat, Navy Rafale N : two seats, Navy
Main differences are:
The difference between Air Force and Navy versions flight model is very light and do not need to be taken into account in F4.
Naval versions (N,M) have only 13 hard points, when Air Force has 14.
Naval version (N,M) front landing gear is different from the land based one, and have a landing hook.
Two seats navy version (N) does not have internal gun (DEFA 30mm) that is on other.
Any plane of every airframe version can be operated with a given “System level”. This concept is different from the U.S. Block system: A F16-C block 40 is the frozen combination of a given airframe and system, this will not change until a complete retrofit (system and airframe). A Rafale M/F1 can be upgraded to F2 standard with only system changes.
As of today, 3 standards are identified: F1: AA only, the today’s (20003-2004) standard of Rafale M
(French Navy) F2: F1 AA: MICA-IR + AG stand off weapons (Scalp-EG and AASM),
first standard for B and C versions (French Air Force)F3: improved AA with Helmet Mounted Cueing System (High Offset Boreseight for MICA-IR), improved AG with Laser Guided weapons (with Damocles Pod) and Nuclear missile ASMPA, Air-Sea capabilities…
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 3 / 55
Basic data
Dry weight : 9,060 kg / 19,973lb (B/C), 9,670 kg / 21,319 lb (M/N)
Max Take Off weight: 24,500 kg Internal Fuel Capacity : 4,750 kg / 5,650 l / 10,500 pounds Reference Area : 45.70 m2 (498 sq.ft) Max Mach Number : 1.8 Max Indicated Air speed (VNE) : 800 Keas Ceil: 55,000 ft Approach speed : 120 Keas Max. Load Factor : +9 / -3.6G (CAT-I); +5.5/-3 (CAT-III)
Engine SNECMA M88-2 Dry Thrust : 50 kN (11,250 lb) AB Thrust: 75 kN (17,000 lb)
Radar: THALES RBE-2, AG (TFR) and AA mode, Multiple targets following (with missile data link allowing firing 2 fox-3 without missile seeker lock, and 6 other fox-3 with lock prior to launch) , Look down-Shoot down, high range (60 Nm for SER of 5 m2, over or under flight level) .
Electronic Counter Measures: Internal (no Pods): SPECTRA combining passive sensor, active jamming and shaff / flare dispensers (4)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 4 / 55
Weapon Loads
Internal Gun: one (right side) DEFA 791B with 125 rounds (fire rate of 2,500 rd/min), for all versions excepted navy twin seat (N).
14 hard points for B and C, 13 for M and N (HP-7 not available)
Rafale F1HP 1 2 3 4 5 6 7 8 9 10 11 12 13 14
Magic-2 1 1MICA-EM 1 1 1 1 1 1RPL-7111250L
1 1 1
RPL-7512000L
1 1 1
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 5 / 55
Rafale F2HP 1 2 3 4 5 6 7 8 9 10 11 12 13 14
Magic-2 1 1MICA-EM 1 1 1 1 1 1 1MICA-IR 1 1 1 1 1 1 1AASM 3 3
SCALP-EG 1 1 1Mk-82 3 3BSU-49 3 3BLU-107B 3 3RPL-7111250L 1 1 1RPL-7512000L 1 1 1
Rafale F3HP 1 2 3 4 5 6 7 8 9 10 11 12 13 14
Magic-2 1 1MICA-EM 1 1 1 1 1 1 1MICA-IR 1 1 1 1 1 1 1AASM 3 3
SCALP-EG 1 1 1Mk-82 3 3BSU-49 3 3BLU-107B 3 3BGL-250 3 3BGL-1000 1 1Laser POD(DAMOCLES) 1
AM-39 1 1AMSP-A 1 1 1RPL-7111250L 1 1 1RPL-7512000L 1 1 1
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 6 / 55
Level Flight EnvelopeRafale
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 7 / 55
0
10,000
20,000
30,000
40,000
50,000
60,000
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
)
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
Mach
Alt
(ft
)
AA2 : GW=14.2tDI=48 : 6xMICAClean : DI=0,
GW=10.3t
AG1 : GW=19.750tDI=203 : 4xMICA+6xGBU-12+2xRPL-571
AA3 : GW=12.6tDI=76 : 4xMICA+2xR550+1250l
Clean : DI=0, GW=10.3t
Level Flight Envelope
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
DATA BASIS : ESTIMATEDCONDITIONS:•Standard Day•MILL Power
Aircraft : Rafale CEngine :SNECMA M88-2E4
AA2 : GW=14.2tDI=48 : 6xMICA
AA3 : GW=12.6tDI=76 : 4xMICA+2xR550+1250l
AG1 : GW=19.750tDI=203 : 4xMICA+6xGBU-12+2x2000l
Max. M
ach number
Max. M
ach number w
ith RP
L-571
Max. M
ach number w
ith RP
L-571
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 8 / 55
Turn PerformanceAircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 9 / 55
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
Maximum Sustained Turn Rate
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
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
35.00
0.00 0.50 1.00 1.50 2.00
Mach number
Max
imu
m in
stan
tan
eou
s tu
rn r
ate
(deg
/s)
0
10,000
15,000
20,000
30,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 10 / 55
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
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
acto
r (N
g)
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
aila
ble
Lo
ad
Fac
tor
(Ng
)
0
10,000
15,000
20,000
30,000
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 11 / 55
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
(de
gre
e p
er s
eco
nd
)
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Turn Performance – Sea Level DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 30.15 deg/s
Max. Sustained Turn = 25.99 deg/s
MA
XIM
UM
AIR
SP
EE
DAircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 12 / 55
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 1.30
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 29.10 deg/s
Max. Sustained Turn = 25.06 deg/s
MA
XIM
UM
AIR
SP
EE
D
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 13 / 55
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 1.30 1.40
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 26.86 deg/s
Max. Sustained Turn = 22.32 deg/s
MA
XIM
UM
AIR
SP
EE
D
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 14 / 55
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 1.40 1.50
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 24.76 deg/s
Max. Sustained Turn = 29.15 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 15 / 55
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 1.40 1.50 1.60
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 22.72 deg/s
Max. Sustained Turn = 16.13 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 16 / 55
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 1.40 1.50 1.60 1.70 1.80
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 20.81 deg/s
Max. Sustained Turn = 13.95 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 17 / 55
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 1.40 1.50 1.60 1.70 1.80 1.90
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 19.06 deg/s
Max. Sustained Turn = 11.92 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 18 / 55
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 1.40 1.50 1.60 1.70 1.80 1.90
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : DEMO•DRAG INDEX = 0•GW=10.3 t
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 16.11 deg/s
Max. Sustained Turn = 9.35 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 19 / 55
Turn PerformanceAircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 •4xMICA + 2xR550 + 1x1250l•GW=27,900lbs / 12.7t•CdVE “A/A” (+9G – AoA < 29)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 20 / 55
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
Maximum Available Turn Rate
0.00
5.00
10.00
15.00
20.00
25.00
30.00
35.00
0.00 0.50 1.00 1.50 2.00
Mach number
Max
imu
m in
stan
tan
eou
s tu
rn r
ate
(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
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
mach number
Su
sta
ined
tu
rn r
ate
de
g/s
0
10,000
15,000
20,000
35,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 21 / 55
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
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
Max
imu
m A
vail
ab
le L
oa
d F
acto
r (N
g)
0
10,000
15,000
20,000
30,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 22 / 55
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
(de
gre
e p
er s
eco
nd
)Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
+500
+750
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 28.39 deg/s
Max. Sustained Turn = 22.33 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 23 / 55
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 1.30
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 26.21 deg/s
Max. Sustained Turn = 19.86 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 24 / 55
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 1.40
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 24.28 deg/s
Max. Sustained Turn = 17.62 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 25 / 55
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 1.40 1.50
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 22.29 deg/s
Max. Sustained Turn = 15.09 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 26 / 55
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 1.40 1.50 1.60
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
+500
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 20.39 deg/s
Max. Sustained Turn = 12.67 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 27 / 55
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 1.40 1.50 1.60 1.70 1.80
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 18.88 deg/s
Max. Sustained Turn = 10.89 deg/s
MA
XIM
UM
AIR
SP
EE
D
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 28 / 55
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 1.40 1.50 1.60 1.70 1.80 1.90
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 30,000 ft DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 16.26 deg/s
Max. Sustained Turn = 9.23 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 29 / 55
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 1.40 1.50 1.60 1.70 1.80 1.90
Mach Number
Tu
rn R
ate
(deg
ree
per
sec
on
d)
Turn Performance – 35,000 ft DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
+250
0
-250
9G
8G
7G
6G
5G
4G
3G
2G
Quickest Turn = 13.11 deg/s
Max. Sustained Turn = 7.18 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
-500
-750
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 30 / 55
Turn PerformanceAircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA < 23)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 31 / 55
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
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
mach number
Su
sta
ine
d t
urn
rat
e 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
0.00 0.20 0.40 0.60 0.80 1.00 1.20
Mach number
Max
imu
m in
sta
nta
ne
ou
s t
urn
ra
te (
de
g/s
)
0
10,000
15,000
20,000
30,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 32 / 55
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
Maximum Available Load Factor
0.00
2.00
4.00
6.00
0.00 0.20 0.40 0.60 0.80 1.00 1.20
Mach number
Ma
xim
um
Av
aila
ble
Lo
ad F
act
or
(Ng
)
0
10,000
15,000
20,000
30,000
Maximum Sustained Load Factor (Ng)
0.00
2.00
4.00
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
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 33 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)
+150
0
-150
-300
+300
9G8G7G6G
5G
4G3G
2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Quickest Turn = 17.11 deg/s
Max. Sustained Turn = 13.51 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 34 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
+300
9G8G7G6G
5G
4G
3G
2G
Quickest Turn = 15.78 deg/s
Max. Sustained Turn = 11.93 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 35 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
+300
9G8G7G6G
5G
4G
3G
2GQuickest Turn = 14.68 deg/s
Max. Sustained Turn = 10.51 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 36 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
9G8G7G6G
5G
4G
3G
2G
Quickest Turn = 13.45 deg/s
Max. Sustained Turn = 8.90 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
-450
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 37 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
9G8G7G6G
5G
4G
3G
2G
Quickest Turn = 12.39 deg/s
Max. Sustained Turn = 7.34 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
-450
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 38 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
9G8G7G6G
5G
4G
3G
2G
Quickest Turn = 11.03 deg/s
Max. Sustained Turn = 6.20 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
-450
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 39 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
+150
0
-150
-300
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 8.96 deg/s
Max. Sustained Turn = 5.15 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
-450
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 40 / 55
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
Mach Number
Tu
rn R
ate
(de
gre
e p
er s
eco
nd
)Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG1•2x RPL 571 + 6xGBU-12 + 4xMICA•GW= 19.7 t•CdvE “Charges” (+6G / AoA<23)
0
-150
-300
9G8G7G6G5G
4G
3G
2G
Quickest Turn = 7.15 deg/s
Max. Sustained Turn = 3.78 deg/s
MA
XIM
UM
MA
CH
NU
MB
ER
(M 0.95)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 41 / 55
Climb Performance
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 42 / 55
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Mach number given best Climb Rate
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA1•2x R550•GW= 11.4 t•CdvE “A/A” (+9G / AoA<29)
0
10,000
20,000
30,000
40,000
50,000
60,000
70,000
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
1.20
1.40
1.60
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
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 43 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Climb Angle
0
100
200
300
400
500
600
700
800
900
1,000
1,100
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
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA1•2x R550•GW= 11.4 t•CdvE “A/A” (+9G / AoA<29)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 44 / 55
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Mach number given best Climb Rate
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA1•2x R550•GW= 11.4 t•CdvE “A/A” (+9G / AoA<29)
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
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
be
r g
ivin
g M
ax
Clim
b R
ate
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 45 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Climb Angle
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA1•2x R550•GW= 11.4 t•CdvE “A/A” (+9G / AoA<29)
0
100
200
300
400
500
600
700
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
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 46 / 55
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Mach number given best 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
)
0.00
0.20
0.40
0.60
0.80
1.00
1.20
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 C
limb
Ra
te
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 47 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Climb Angle
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
0
100
200
300
400
500
600
700
800
900
1,000
1,100
1,200
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 48 / 55
Maximum Instantaneous Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Mach number given best Climb Rate
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
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
)
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
nu
mb
er
giv
ing
Ma
x C
limb
Ra
te
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 49 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Climb Angle
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AA3 / DI = 76 4xMICA + 2xR550 + 1x1250lGW=27,900lbs / 12.7tCdVE “A/A” (+9G – AoA < 29)
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 1.50 1.60 1.70 1.80 1.90 2.00
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 50 / 55
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG12x RPL 571 + 6xGBU-12 + 4xMICAGW= 19.7 tCdvE “Charges” (+6G / AoA<23)
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
)
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
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 51 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG12x RPL 571 + 6xGBU-12 + 4xMICAGW= 19.7 tCdvE “Charges” (+6G / AoA<23)
Climb Angle
0
100
200
300
400
0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 52 / 55
Maximum Instantaneous Climb Rate
Mach number given best Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG12x RPL 571 + 6xGBU-12 + 4xMICAGW= 19.7 tCdvE “Charges” (+6G / AoA<23)
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
nu
mb
er g
ivin
g M
ax
Clim
b R
ate
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 53 / 55
Climb Rate
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•MIL Power
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS : AG12x RPL 571 + 6xGBU-12 + 4xMICAGW= 19.7 tCdvE “Charges” (+6G / AoA<23)
Climb Angle
0
100
200
300
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
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 1.50 1.60 1.70 1.80 1.90 2.00
Mach
Clim
b A
ng
le (
deg
)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 54 / 55
Acceleration Performances
Rafale C
Rafale’s Flight Model by J.M. LANGERONVersion: 2006.346
Page 55 / 55
0
20
40
60
80
100
0.50 1.00 1.50 2.00Mach
Tim
e (s
)
0
30
60
90
120
150
180
0.50 1.00 1.50 2.00
Mach
Tim
e (s
)Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:•Standard Day•Max AB
Aircraft : Rafale CEngine :SNECMA M88-2E4
CONFIGURATIONS :•DRAG INDEX = 14 (2xR550)•GW=11.4t
10,000 ft20,000 ft
30,000 ft
45,000 ft
36,000 ft
Sea Level
Recommended