Aero S-103 (Mig-15bis)

Modern Drawings/Air/Czechoslovakia/Fighters/MiG-15//S-102.htm | Update: -

MiG-15bis jet fighters built under license in Czechoslovakia with Motorlet M-06 (licensed VK-1) engines.
CzAF - Caslav, 1957.

Specifications

General

Type: Fighter
Crew: 1
First flight: 30 December 1947
Introduction: 1949
Production: 13130 in the USSR + at least 4180 under license

Powerplant

1 × Klimov VK-1 centrifugal-flow turbojet
Dry thrust: 26.5 kN
Thrust with afterburner: -

Dimensions/Masses

Length: 10.102 m | Wingspan: 10.085 m | Height: 3.7 m
Wing area: 20.6 m² | Empty weight: 3681 kg
Max. takeoff weight: 6106 kg

Performances

Maximum speed: : Mach 0.9 (1107 km/h)
Service ceiling: 15500 m
Range: 2520 km with 2x600 L drop-tanks

Armament

Inside: 1 × 37 mm Nudelman N-37 autocannon with 40 rounds, 2 × 23 mm Nudelman-Rikhter NR-23 autocannon with 160 rounds
Outside: 2 Hard points with provisions to carry combinations of:
Bombs: 100 kg bombs
Other: drop tanks, or unguided rockets