Prévoyance Labbe: Difference between revisions
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The '''Prévoyance Labbe''' (English: ''Prévoyance Skua'') is a single seat, two engine, all weather, {{wpl|fourth-generation fighter jet|fourth generation}}, {{wpl|Multirole combat aircraft|multirole fighter}}. The Labbe is designed to conduct a variety of air combat missions including {{wpl|aerial warfare|air superiority}}, {{wpl|attack aircraft|ground attack}}, {{wpl|naval aviation|maritime strike}} and {{wpl|nuclear warfare|nuclear strike}}. The Labbe is currently produced in three variations the M {{wpl|CATOBAR|conventional carrier based}}, C {{wpl|CTOL|conventional take-off and landing}}, R {{wpl|Aerial reconnaissance|reconnaissance}} models. | The '''Prévoyance Labbe''' (English: ''Prévoyance Skua'') is a single seat, two engine, all weather, {{wpl|fourth-generation fighter jet|fourth generation}}, {{wpl|Multirole combat aircraft|multirole fighter}}. The Labbe is designed to conduct a variety of air combat missions including {{wpl|aerial warfare|air superiority}}, {{wpl|attack aircraft|ground attack}}, {{wpl|naval aviation|maritime strike}} and {{wpl|nuclear warfare|nuclear strike}}. The Labbe is currently produced in three variations the M {{wpl|CATOBAR|conventional carrier based}}, C {{wpl|CTOL|conventional take-off and landing}}, and R {{wpl|Aerial reconnaissance|reconnaissance}} models. | ||
==History and Development== | ==History and Development== | ||
Revision as of 19:01, 23 April 2020
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| Prévoyance Labbe | |
|---|---|
| |
| Labbe of Flottille F15 taking off from the NNS Triomphe | |
| Role | Air superiority, Multirole combat aircraft |
| National origin |  Notreceau
|
| Manufacturer | Prévoyance |
| Designer | Prévoyance |
| First flight | July 5th, 1985 |
| Introduction | April 3rd, 1996 |
| Status | In service |
| Primary users | Notreceauen Airforce Notreceauen Navy |
The Prévoyance Labbe (English: Prévoyance Skua) is a single seat, two engine, all weather, fourth generation, multirole fighter. The Labbe is designed to conduct a variety of air combat missions including air superiority, ground attack, maritime strike and nuclear strike. The Labbe is currently produced in three variations the M conventional carrier based, C conventional take-off and landing, and R reconnaissance models.
History and Development
Design
Specifications
General characteristics
- Crew: 1
- Length: 50.01 ft (15.27 m)
- Wingspan: 35.9 ft (10.9 m)
- Height: 17.5 ft (5.34 m)
- Wing area: 492 ft² (45.7 m²)
- Empty weight: 22,708 lbs (10,300 kg)
- Loaded weight: 54,013 lbs (24,500 kg)
- Max. takeoff weight: 54,013 lbs (24,500 kgs)
- Powerplant: 2 × Solaire M1008-54 derivative afterburning turbofan
- Dry thrust: 22,500 lbf (100.08 kN) each
- Thrust with afterburner: 34,000 lbf (150 kN) each
Performance
- Maximum speed:
- At sea level: Mach 1.1
- At altitude: Mach 1.8
- Combat radius: 1,150 mi (1,000 nmi, 1,850 km)
- Service ceiling: 49,984 ft (15,253 m)
- Rate of climb: 60,000 ft/min (304.8 m/s)
- Maximum g-load: +9.0 g
Armament
- Guns: 1 x GIST 30 30 mm autocannon
- Hardpoints: 14 for C variant 13 for M variant with a capacity of up to 20,900 lb (9,500 kg) of stores
- Missiles:
- Bombs:
- B.547 340 kg (7,50 lbs) guided bombs
- BD.206 cluster bomb
- BD.1012, BD.1011, and BD.1010 general-purpose bombs
- BD.351, BD.352, BD.353 laser-guided bombs