Weiss WM-21 Sólyom
|Role||Light Bomber/Reconnaissance Biplane|
|Developed from||Weiss WM-16 Budapest|
Design and development
The WM-21 was designed as an simplified variant of the WM-16 for service use, the structure was strengthened and refined and the tailwheel was replaced with a tailskid to allow for shorter landing runs on grass airfields. A conventional biplane, the Sólyom was powered by a 870 hp (649 kW) Weiss WM-K-14A radial engine. A total of 128 aircraft were built by three different factories, Manfred Weiss built 25, 43 by MAVAG and 60 by MWG.
The first aircraft entered service in 1939 with short-range reconnaissance units, although active during the 1940 dispute with Romania their first active operational use was during the Axis invasion of Yugoslavia in August 1941. From June 1941 they were used to support Hungarian Army units in the Ukraine and then against Soviet partisans. Around 80 aircraft were also transferred to duties as trainers, as they were removed from operational use, until 1945.
- Crew: 2
- Length: 9.64 m (31 ft 8 in)
- Upper wingspan: 12.90 m (42 ft 4 in)
- Lower wingspan: 9.40 m (30 ft 10 in)
- Height: 3.5 m (11 ft 6 in)
- Empty weight: 2,300 kg (5,071 lb)
- Gross weight: 3,400 kg (7,496 lb)
- Powerplant: 1 × Weiss WM-K-14A radial, 650 kW (870 hp)
- Maximum speed: 320 km/h (199 mph; 173 kn)
- Range: 750 km (466 mi; 405 nmi)
- Guns: 3 x 7.9mm (0.31in) Gebauser machine-guns
- Bombs: 12 x 10kg (22lb) Anti-personnel bombs and 120 x 1kg (2.2 lb) incendiary bombs
- Orbis 1985, p. 3079
- "AWM-21 Sólyom". Retrieved 28 January 2012.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.