Description

The Reimerrten RR-20M-1C was an upgrade to the first production RR-20M, the new variant was based on the design of the carrier based RR-20M-1B with some slight changes, along with some weight reduction done to enhance the aircraft performance.

Role - Multi-Role Air Superiority Fighter

First flight - 12 April 1973

Introduction - February 1975

Primary user - Oslavian Airforce

Specifications

General characteristics

Crew: 1
Length: 19 m
Wingspan: 12 m
Height: 5 m
Wing area: 71.1 m²
Empty weight: 13,000 kg
Gross weight: 30,375 kg
Max takeoff weight: 39,450 kg
Fuel capacity : 10,000L internal + 2 × 2,500L drop tank + 1 × 5,000L drop tank and 2 × 2,500 litre CFT's
Powerplant: 2 × Afterburning Turbofan engines, 117.6 kN (12,000 kgf) thrust each dry, 196.1 kN (20,000 kgf) with afterburner

Performance

Maximum speed: Mach 3.2
Combat Range: 1,500 km (internal fuel)
2,500 km (with CFT)
5,000 km (with CFT & 2 × 2,500L drop tanks and 1 × 5,000L drop tank)
Ferry range: 5,000 km (internal fuel)
7,500 km (with CFT)
12,500 km (with CFT & 2 × 2,500L drop tanks and 1 × 5,000L drop tank)
Service ceiling: 25,000 m
Wing loading: 569.4 kg/m²

Armament

1 × 20mm rotary cannon

Hardpoints: Total 9: two under-wing (each with additional two missile launch rails), four under-fuselage and a single centerline pylon station, optional fuselage pylons (which may include conformal fuel tanks)

Controls

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