Turbine Sound Studios proudly presents the HD version of the Airbus 380 Rolls Royce Trent-900 soundpack for FS2004 recorded in HD High definition.
This soundpackage is spcific developed for use with the Project Airbus A380, but will work with other models ( Small variations can occour )
This soundpackage includes the following :
- External engine sounds
- Internal engine sounds
- Gear sounds
- Wind sounds
- Cockpit environment sound
- Rolling and rumble cabin sound
The Airbus A380 is a double-deck, wide-body, four-engine jet airliner. It is the world's largest passenger airliner; many airports have upgraded their facilities to accommodate it because of its size. Initially named Airbus A3XX, Airbus designed the aircraft to challenge Boeing's monopoly in the large-aircraft market; the A380 made its first flight on 27 April 2005 and began commercial service in October 2007 with Singapore Airlines.
The A380's upper deck extends along the entire length of the fuselage, with a width equivalent to a wide-body aircraft. This gives the A380-800's cabin 478 square metres (5,145.1 sq ft) of floor space; with 49% more floor space than the next-largest airliner, the Boeing 747-8, the cabin provides seating for 525 people in a typical three-class configuration or up to 853 people in all-economy class configurations. The A380-800 has a design range of 15,700 kilometres (8,500 nmi; 9,800 mi), sufficient to fly from New York to Hong Kong, and a cruising speed of Mach 0.85 (about 900 km/h or 560 mph; 490 kn at cruising altitude).
As of July 2013, Airbus has received 262 firm orders and delivered 106 aircraft.
Emirates has ordered the most A380s with 90.
Specifications (Trent 900)
General characteristics
Type: Three-shaft high bypass ratio (8.7-8.5) turbofan engine
Length: 4.55 m (179 in)
Diameter: 2.94 m (116 in) fan tip
Dry weight: 6,271 kg (13,830 lb)
Components
Compressor: Eight-stage IP compressor, six-stage HP compressor
Combustors: Tiled combustor
Turbine: Single-stage HP turbine, single-stage IP turbine, five-stage LP turbine
Performance
Maximum power output:
Overall pressure ratio: 37-39
Thrust-to-weight ratio: 4.93-5.63 (assuming 14,190 lb (6,440 kg) weight of engine and certified to 70,000–80,000 lbf or 310–360 kN of thrust)
PLEASE NOTE : Sound quality can be reduced in the promotion video ( Video converting )
