| General |
|
| Type |
C-390 |
| Popular
designation |
Millennium |
| Versions |
C-390,
KC-390 |
| Prototype |
|
| Project
name |
|
| Design
organisation |
Embraer
(Brazil) |
| Main
secundary design organisations |
International
Aero Engines |
| Production
organisation |
Embraer
(Brazil) |
| Primary
task |
Multi-mission
|
| Type
aircraft |
Military
tactical transport |
| Specials |
|
| Length |
62
ft. 1 in. (18.9 meters) |
| Height |
16
ft. 8 in. (5.1 meters) |
| Wingspan |
44
ft. 6 in. (13.6 meters) |
| Wing
surface |
78.04
square meters |
| Aspect
ratio |
|
| Sweep
back |
|
| Dihedral |
|
| Performance |
|
| Engines |
2x
IAE V2500-E turbofan engines |
| Thrust |
31,330
lb (each) |
| Weight
(empty) |
|
| Weight
(start, maximum, MTOW) |
|
| Weight
(landing, maximum, MLW) |
|
| Required
runway length (start) |
1165m
(3820 ft) with 16 ton payload
1524m (5000 ft) with 23 ton payload |
| Required
runway length (landing) |
1000m
(3280 ft) with 26 ton payload |
| Cruise
speed |
120
KCAS to 300 KCAS |
| Maximum
speed |
470
KTAS (Mach 0,8) |
| Ceiling |
36,000
ft |
| Maximum
range |
4570
nm (ferry flight with internal tanks)
3370 nm (ferry flight)
1470 nm (23 ton payload)
1080 nm (26 ton payload
|
| Fuel
capacity |
|
| Air-to-air-refueling
capability |
|
| Passengers |
|
| Payload |
Possible
combination of:
- 26 ton (57,320 lb)
- 463L pallets
- A-22 CDS bundles
- Low Velocity Aerial Delivery (LVAD) type V platforms
- Aerial delivery of CDS
- up to 22 skid boards (Low Altitude Parachute Extraction (LAPES)
- Four spotter positions, Lateral litters and/or crew seats
- 74 Litters (STANAG 2040) and 8 additional member including medical
attendants and necesary life supporting equipment |
| Length
cargo hold |
18.50m
(60 ft 8 in) (including ramp) |
| Useful
cargo hold length |
|
| Useful
cargo hold width |
3.45m
(11ft 4 in) |
| Useful
cargo hold height |
2.95m
- 3.2m (9ft 8 in - 10 ft 6 in) |
| Volume |
169
kubic meters (5970 kubic ft) |
| Equipment |
|
| Armament |
Possible
combination of:
- Chaff & Flare |
| Maximum
weapon load |
|
| Maximum
G resistance |
|
| Radar |
Selex
Galileo Gabbiano Tactical Radar T-20 |
| Sensors |
Possible
combination of:
- Rafael Litening II electro-optical infrared targeting pod
- Radar Warning Receiver
- Laser Warning Receiver
- Missile Approach Warning System (MAWS)
- Directional InfraRed Counter Measures (DIRCM)
- Enhanced Vision System (EVS) |
| Avionics |
Possible
combination of:
- Rockwell Collins Pro Line Fusion Avionics System |
| Other
equipment |
Possible
combination of:
- Cobham 900E Series Wing Air Refueling Pod
- Internal fuel tanks
- Ballistic Protection (Armor 7.62mm and 0.50 inch)
- HALO Oxygen Rack
|
| Type
flight controls |
|
| Landing
gear |
|
| Usage |
|
| Manufactured |
|
| Crew |
|
| Costs |
|
| First
flight |
|
| First
delivery |
|
| Operational
since |
|
| Successor
of |
C-130H
(Netherlands) |
| Replaced
by |
|
| Comparable
aircraft |
C-130J |
| Operators
(current and future) |
Hungary,
Netherlands, Portugal |
| Main
operators |
|
| Amphibious
usage |
No |
| Status |
In
production, in operational service |