The MB-339 Family

MB-339
Evoluzione di un progetto
COMPANY CONFIDENTIAL
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MB-326
MB-339A
MB-339PAN
MB-339CB
MB-339CD/FD
MB-339A/PAN MLU
COMPANY CONFIDENTIAL
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The MB-339 Family
Key Features
MB-339 customers
• Initial design based on the Italian Air Force
requirement for a state-of-the-art jet trainer
• In service with nine military operators
DUBAI
ERITREA
GHANA
ITALY
MALAYSIA
NIGERIA
PERU’
NEW
ZEALAND
ARGENTINA
worldwide
• Most cost/effective advanced/lead-in fighter
trainer
• Excellent capabilities as a Light Combat
Aircraft
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MLU – MID LIFE UPGRADE
ELT &
UAB
Luci di
formazione
Upgrade
strutturale
Batterie in
parallelo
Airborne Strain
Counter
Upgrade
avionico
Crash
Data Rec.
Modifiche
manetta
Supporto per
IFF MOD 4
Nuova radio
V/UHF
Sostituzione materiali obsoleti
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MB-339CD Platform Description
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Technical Data & Performance
•
•
Empty weight
3,330 kg / 7,350 lb
Take-off weight, clean
4,950 kg / 10,900 lb
Max. take-off weight (armed)
6,350 kg / 14,000 lb
Engine
Rolls-Royce Viper 632
Thrust
1,815 kg
Max. level speed (s.l.)
470 kts
Specific Excess Power (*)
6,450 ft/min
Max. load factor
+ 7.33 / - 4 g
Max. sustained load factor (*)
Take-off run, clean (s.l., ISA)
Time to 20,000 ft, ISA
+ 5.1 g
620 m / 2,035 ft
4.8 min
Note : (*) = s.l., ISA, 50 % fuel
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Main Systems
Avionics
•
Glass Cockpit
(Head-Up Display &
3 LCD-MFD each cockpit)
•
Stores Management System
•
HOTAS Controls
•
Ring Laser Gyro Platform with
embedded Gps
•
Mission Processor
INSTRUMENTS AND CONTROLS FULLY DUPLICATED IN THE REAR COCKPIT
Instructor Override for:
Trim and Airbrake
Gun Firing
Weapon Delivery
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Technical Data & Performance
• Take-off weight, clean
• Max. level speed (s.l.)
• Max. load factor
4,950 kg / 10,900 lb
470 kts
+8/-4g
Flying Qualities
• Predictable flying qualities
• Student error tolerance:
Spin resistant
Benign stall characteristics
• Easy and standard recovery from both
erected and inverted spin
• Maneuverable and stable firing platform
COMPANY CONFIDENTIAL
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Evolution of the MB-339 Family
MB-339A / B
• Conventional Avionics and
Cockpit Layout
MB-339C
MB-339CD
• Digital Avionics (ARINC 429)
• Digital Avionics (MIL-STD-1553B)
• 2 HUDs
• 2 HUDs
• Strap-down Inertial Platform & Doppler
Velocity Sensor
• Ring Laser Gyro Platform with
embedded GPS
• 1 Navigation Computer
• 1 Weapon Aiming Computer
• 1 Computer for Navigation and Attack
(Central Mission Processor)
• 1 mono-chromatic MFD
• 3 Colour Liquid Crystal MFD
• HOTAS
MB-339 improved through more than 500,000 FH
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Avionic Cockpit Layout
F-18
MB-339CM
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Training Capabilities
Night Operations Capabilities
INTERNAL / EXTERNAL LIGHTING COMPATIBLE WITH NIGHT VISION GOGGLES (NVG’S GEN III)
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Main Systems
Avionics
MAIN COMPUTER
SENSORS
DISPLAYS
LINKS
•
•
Mission Processor for navigation, weapon aiming, HUD symbology generation
•
•
•
•
•
•
•
Ring laser gyro platform with embedded GPS
•
MIL-STD-1553B Digital Information Distrib. System
Digital Map Generator for map symbology generation, mission & maintenance
data recording
Radar Altimeter
Air Data Computer
VOR/ILS + TACAN ( + ADF + DF )
HUD with up-front control panel in both cockpits
Three 5”x 4” LCD smart MFDs / NVG compatibility
Dedicated display for Communication / IFF
Flexible system based on modular approach & open architecture
COMPANY CONFIDENTIAL
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Main Systems
MFD Formats
MENU
DISP
17
F/ D
180
MENU
C-ADI
18
19
20
21
DISP
R1850
MILES
CRS
9
3. 2
191
8
CUT
ARM
7
30
SMS
RKT
RELOAD
6
160
2500
4
148
– 0. 3
140
3
2 380
1
2000
–3 0
GUN
9
RKT
RESET
25
RKT
25
SEL
JETT
BRD
GS
RNAV I LS
MENU
DISP
ILES
CRS
19 . 3
304
30
AUTO
BAP
6
SI M
8
5200
988. 7
LOC
BRD
6
BAP
6
2
120
LAT
GUN
125
BAP
33
MAP
HSI
N
24
03
21
06
E
S
GS 341
WD 062 / 7
RNAV BRD
15
12
TTG
3.4
FTG
40
X075 TACAN
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Main Systems
HOTAS Controls
ENGINE THROTTLE
NAV.ATTK / DOGFIGHT
CONTROL STICK
UNCAGE / LG DOWN
SIGNAL TRANSMISSION
CCRP TARGET
DESIGNATION /
MARK
WEAPON
RELEASE
RADIO PTT
TRIM
RADIO PTT
GUN FIRING
SPEED BRAKE
ENGINE RELIGHTING
NOSEWHEEL
STEERING / BARO FIX
DESIGNATION
TARGET DESIGNATOR POSITION CONTROL /
STADIAMETRIC RANGE CONTROL
COMPANY CONFIDENTIAL
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Main Systems
In flight refueling system
• First western trainer equipped with an in-flight refueling system
• Probe and drogue system (used by U.S. Navy and major NATO Air
Forces)
• Fuel transfer capability: 200 kg/min
• Quick probe installation / removal (less than 20 minutes)
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Main Systems
In flight refueling system
Higher Operational Flexibility
Radius of action
Loitering Time
Higher training effectiveness
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Main Systems
Escape System
Two zero-zero Martin Baker MK10L
seats
Emergency transparency breaking on
the ground by explosive chord
Ejection commanded either in
sequence from the rear seat or
independently by the two pilots
(mode manually set before flight)
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Operational Capabilities
MARTE MK-2A Anti-Ship Missile
OTO MELARA
MKMK-2A MARTE
AIRAIR-TOTO-SHIP MISSILE
AIM-9L Sidewinder Missile
AIMAIM-9L SIDEWINDER
MISSILE
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