Prévoyance Héron Noir
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| Prévoyance Héron Noir | |
|---|---|
| |
| Héron Noir demonstrator at Le Aigle Airshow, 2013 | |
| Role | Air superiority, Multirole combat aircraft |
| National origin |  Notreceau  Ostlichtor  Pequenoya
|
| Manufacturer | Prévoyance |
| Designer | Prévoyance |
| First flight | October 7th, 2011 |
| Introduction | November 11th, 2017 |
| Status | In service |
| Primary users | Notreceauen Airforce Notreceauen Navy |
The Prévoyance Héron Noir (English: Prévoyance Black Heron) is a single-seat, single-engine, all weather fifth generation multirole fighter with stealth capabilities. The Héron Noir is designed to conduct a variety of air combat missions including air superiority, ground attack and maritime strike. The family of Héron Noir aircraft include three models: Héron Noir M conventional carrier based, Héron Noir C conventional take-off and landing and the Héron Noir SJ short take-off and landing model.
In 1999 the National Directorate of Notreceau initiated the Programme de chasse de nouvelle génération (Next Generation Fighter Program) with the aim of fielding a new 5th generation fighter that would incorporate stealth technologies into its design and would specialize in strike missions. In 2001 Prévoyance was chosen as the primary design company to proceed with the project and began to develop prototypes and technology demonstrators. Following significant cost overruns during research and development a proposal to extend the program to several partner nations in 2003 was approved by the Department of Defense Research and Development. After several proposals the program was extended to include Saab-Volvo, [West March Company] and [Yisrael Company] to help shoulder development costs and increase production capacity for the new aircraft in 2005.
History and Development
Design
Specifications
General characteristics
- Crew: 1
- Length: 45.01 ft (13.72 m)
- Wingspan: 36 ft (10.97 m)
- Height: 17.32 f (5.28 m)
- Wing area: 590 ft² (54.8 m²)
- Empty weight: 22,490 lbs (10,201 kg)
- Loaded weight: 38,966 lbs (17,675 kg)
- Max. takeoff weight: 41,500 lbs (18,824 kgs)
- Powerplant: 1 × Solaire M2012-77 derivative afterburning turbofan
- Dry thrust: 28,000 (125 kN)
- Thrust with afterburner: 43,000 lbf (191 kN)
Performance
- Maximum speed:
- At sea level: Mach 1.1
- At altitude: Mach 1.6
- Combat radius: 978 mi (850 nmi, 1,574 km)
- Service ceiling: 50,000+ ft (15,240+ m)
- Rate of climb: 50,000 ft/min (254 m/s)
- Maximum g-load: +9.0 g
Armament
- Guns: 1 x GIST 30 30 mm autocannon
- Hardpoints: 6 × external pylons on wings with a capacity of 15,000 lb (6,800 kg) and two internal bays with a capacity of up to 5,700 lb (2,590 kg). with a capacity of up to 15,000 lb (6,800 kg) of stores
- Missiles:
- Bombs:
- BD.2521 340 kg (7,50 lbs) guided bombs
- BD.2642 cluster bomb
- BD.2623, BD.2622, and BD.2621 general-purpose bombs
- BD.2721, BD.2722, BD.2723 laser-guided bombs