
Mirage 2000B | |
|---|---|
| Pays | France |
| Type | Avion d’attaque |
| Description | Album de 36 photos walk-around d’un Mirage 2000B |
Galerie de photos d’un Mirage 2000B , Le Mirage 2000 est un avion militaire conçu par la société Français Dassault Aviation à la fin des années 1970. Version Mirage 2000B: entraînement biplace. Source: Wiki
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General Overview
| Rôle | Conversion Trainer / Combat Trainer |
|---|---|
| National Origin | France |
| Fabricant | Dassault Aviation |
| Crew | 2 (Instructor and Trainee/Pilot) |
| Introduction | Early 1980s (First two-seat flight was October 1980) |
| Relationship to 2000C | Training counterpart to the single-seat 2000C fighter. |
Technical Differences from 2000C
| Length | 14.55 m (Slightly longer than 2000C due to second cockpit) |
|---|---|
| Internal Cannon | Lacks the internal 30 mm DEFA cannons of the 2000C. |
| Fuel Capacity | Reduced internal fuel capacity to accommodate the second seat and controls. |
| Armement | Maintains most hardpoints and the ability to carry a combat load for training purposes. |
| moteur | SNECMA M53-P2 turbofan (Same powerful engine as the 2000C fighter) |
| Avionics/Radar | Equipped with the same or similar fire control radar (like the RDI or RDM, depending on batch) as its single-seat counterpart. |
Primary Function: The main role of the Mirage 2000B is to transition pilots from jet trainers to the high-performance delta-wing fighter. It is fully capable of most combat missions, especially air-to-air interception, but is primarily used for training due to its two-seat configuration.
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