AFASF-12 Drago Air Superiority Fighter

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Ersilia AFASF-12 Drago
AFASF12Drago.jpg
An AFASF-12NG during the SAF international air show in 2018.
General information
TypeAir Superiority Fighter
Multirole Fighter
ManufacturerErsilia Defense and Aeronautics
StatusActive
History
Manufactured1983—Present
Introduction date11 February 1983

The Ersilia AFASF-12 Drago (Dragon) is a single-seat, twin-engine jet fighter designed in Cacerta for the Cacertian Royal Air Fleet. Developed by Ersilia Defense and Aeronautics primarily as an air superiority fighter, it has served as the main air-to-air fighter aircraft of the Air Fleet since its introduction in 1983. They have been consistently upgraded since their introduction and currently feature improved engines, modern radar and IRST sensors, an increased fuel capacity, and HOTAS flight controls.

Although originally designed to fight enemy aircraft, they were later equipped with a range of air-to-surface and precision munitions. As air-to-air missions have become less prevalent in the modern era, many of the Dragos have undergone a refit that has allowed them to also serve as multirole fighters (Drago IIs), although the technical designation of AFASF-12 remains.

The Drago became a popular export aircraft since it’s introduction with purchases made by several nations throughout Tyran. It currently serves as the main air-superiority fighter of the Imperial Shalumite Air Force, the primary combat aircraft of the GASDF, and previously with the Azurlavaian Luftforsvaret. As of 2017, the Drago was still in production officially making it Ersilia’s most produced aircraft to date.

Development

Design

Production

Production Figures

Operational History

Variants

AFASF-12

The initial production version that entered service with the Royal Air Fleet in 1983. Following an upgrade and refit program (which resulted in the AFASF-12A) in the mid-1990s, only a handful of examples of the original version of the Drago currently exist, most of which are listed in the Air Fleet’s reserve or are preserved in museums.

AFASF-12E

The AFASF-12E (Esportazione) is the export variant of the original Drago. Many of the features remain the same between the original and the export, the only differences being a commercial variant, and not the Air Fleet standard, radar and electronic suite.

AFASF-12A

In 1993, Ersilia began a program designed to upgrade the systems of the Drago to modern standards and equipment; the final product was designated as the AFASF-12A (Aggiornamento). A number of flight control improvements provided better stability and controllability as well as an improved mechanical-hydraulic flight control system. The package also included a new radar and ECM system as well as the ability for the Drago to carry underwing and centerline drop tanks for increased range. The AFASF-12A was the first of the Drago family capable of engaging ground targets, although its overall focus was still air-to-air dominance.

AFASF-12EA

Ersilia offered a limited upgrade program to its export customers in 1998 following the success and release of the AFASF-12A designated as the AFASF-12EA (Esportazione Aggiornata). Many of the improvements that were installed on the As were included in the package, however the radar and electronic suits were once again commercial and not the Air Fleet’s standard.

AFASF-12NG

The lack of air-to-air engagements in the modern era resulted in the creation of the newer AFASF-12NG (Nuova Generazione). Originally, the NGs (later nicknamed Drago IIs) were simply further upgraded AFASF-12As with expanded ground attack capabilities. As of 2008, however, the AFASF-12NG entered its own serialized production and NGs that are now entering service are considered brand new aircraft.

Operators

Current Operators

Former Operators

  • Azurlavai; Luftforsvaret—~200 units in service between 1983 and 1987. Placed into reserve and eventually sold.

Specifications (AFASF-12NG)

Ersilia AFASF-12 line drawing.

General Characteristics

  • Crew: 1
  • Length: 17.37 m (57 ft)
  • Wingspan: 11.4 m (37 ft 5 in)
  • Height: 4.73 m (15 ft 6 in)
  • Wing Area: 38 m² (409 ft²)
  • Empty Weight: 13,380 kg (29,500 lbs)
  • Loaded Weight: 19,200 kg (42,330 lbs)
  • Max Takeoff Weight: 26,500 kg (58,420 lbs)
  • Powerplant: 2 × EDA-2010 Afterburning Turbofans
  • Fuel Capacity: 4,200 kg (9,260 lbs)

Performance

  • Maximum Speed: Mach 2.25 (2,100 km/h, 1,310 mph) at altitude
  • Cruise Speed: 1,960 km/h (1,220 mph)
  • Service Ceiling: 16,200 m (>53,000 ft)
  • Rate of Climb: 330 m/s (65,000 ft/min)
  • Wing Loading: 442 kg/m² (90.5 lb/ft²)
  • Thrust/Weight: 1.02

Armament

  • Guns: 1 × 30 mm cannon with 150 rounds
  • Payload: 5,500 kg (12,100 lb) on 10 external hardpoints (10 underwing)