Description

The Va F-11 is a light single-engine supersonic multirole fighter aircraft made to suplement the much more expensive and heavier RR-20M. The Va F-11 has a delta wing and canard configuration with relaxed stability design and fly-by-wire flight controls.

F-11 firing an AAM-02 BVR missile

Role - Multi-Role Fighter

First flight - April 1973

Introduction - February 1977

Primary user - Oslavian Airforce

Specifications

Va F-11 Taxiing on the runway

General characteristics

Crew: 1
Length: 14.5 m
Wingspan: 8.5 m
Height: 5 m
Wing area: 40.6 m²
Empty weight: 6,500 kg
Loaded weight: 10,750 kg
Max takeoff weight: 16,000 kg
Fuel capacity : 5,000L internal + 1 × 2,500L drop tank
Powerplant: 1 × Afterburning Turbofan engines, 58.84 kN (6,000 kgf) thrust dry, 98.06 kN (10,000 kgf) with reheat

Performance

Maximum speed: Mach 2.1
Combat Range: 750 km (internal fuel)
1,500 km (2,500L drop tank)
Ferry range: 2,500 km (internal fuel)
3,750 km (with 2,500L drop tank)
Service ceiling: 20,000 m
Wing loading: 362.5 kg/m²

Armament

2 × 20mm revolver cannons

7 × hardpoints (1 under-fuselage, 4 under-wing and 2 on the wing tips)

Controls

Regular Controls (Joystick/WASD)
AG1 - refuel droge
AG3 - arresting hook
AG4 - jettison drop tanks
AG7 - Drag Chute