MIRAGE 2000
| Subject: | MIRAGE 2000 |
| Update Date: | 2008-11-11 11:16:23.0 |
| Valid Period: |
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Description
The Mirage 2000 was developed by Dassault-Breguet for the Armée de l'Air as an alternative to the swing-wing Avion de Combat Futur. After the latter was cancelled in 1975 due to its growing cost and complexity, Dassault offered the Mirage 2000 as an alternative. Development of this aircraft would also give the company a competitor to the General Dynamics F-16 Fighting Falcon, which had defeated the Dassault Mirage F1 in a contest for a new fighter for the air forces of Belgium, Denmark, Netherlands and Norway.
Specification:
- Wingspan: 632mm (25 in)
- Overall Length: 970mm (38.3 in)
- Flying Weight: 520g (19 oz)
- Wing Loading: 26g/dm²
- Wing Area: 5dm²
- Drive System: 64mm Ducted Fan (Inrunner Brushless Motor (170 watt input)
- Servo: 3X 9g high speed micro servos
- Speed Controller: 20 Amp Brushless Speed Control with Heatsink
- Battery: 11.1V 1200mah Li-Polymer
- Control system: 4 CH Multifunctional FM Radio Transmitter and 6 CH Micro Receiver
- Radio Control Range: 3000 feet (1000m)
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