Aero A.30

A.30

Role	Light reconnaissance bomber
National origin	Czechoslovakia
Manufacturer	Aero
Number built	79 (+116 A.32)
Developed from	Aero A.11
Variants	*Aero A.100 Aero A.32
Developed into	Aero A.100

The Aero A.30 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia in the late 1920s. It originated as an attempt to improve the performance of the Aero A.11, but soon evolved into quite a different aircraft, larger and more powerful than its predecessor. The aircraft is readily distinguished from other related types by the difference in spans between its wings - the upper set being of much greater span than the lower.

Prototypes of the A.30 were retrospectively designated A.130, with the A.230 the main production version. The A.330 and A.430 featured different, more powerful engines, but the latter of these did not enter production, serving instead as the prototype for the Aero A.100.

Variants

A.30: Prototype of a light bomber reconnaissance aircraft, powered by a 372.8 kW (500 hp) Skoda L radial engine.
A.32: Also derived from the A.11, the A.32 was a light reconnaissance bomber powered by a 335.6 kW (450 hp) Walter Jupiter; 116 aircraft built in several versions. Finnish Air Force examples were powered by 372.8 kW (500 hp) Isotta-Fraschini Asso 500 V-12 engines
A.130: Re-engined with a 372.8 kW (500 hp) Bristol Jupiter VI.
A.230: The main production variant; a two-seat bomber powered by a W-12 Lorraine 12Eb Courlis engine.
A.330: Re-engined with a 484.7 kW (650 hp) Praga ESV
A.430: Powered by a Avia Vr-36, the A,430 served as the prototype of the Aero A.100
A.100

Operators

Czechoslovakia

Czechoslovak Air Force

Imperial Iranian Air Force purchased one Aero A.30 from Czechoslovakia in 1923

Specifications (A.230)

General characteristics

Crew: 2 (pilot & observer)
Length: 10 m (32 ft 10 in)
Wingspan: 15.3 m (50 ft 2 in)
Wing area: 46.2 m² (497 sq ft)
Empty weight: 1,420 kg (3,131 lb)
Gross weight: 2,375 kg (5,236 lb)
Powerplant: 1 × Lorraine 12E Courlis W-12 water-cooled piston engine, 340 kW (450 hp)

Performance

Maximum speed: 198 km/h (123 mph; 107 kn)
Service ceiling: 5,800 m (19,029 ft)
Rate of climb: 3.083 m/s (606.9 ft/min)
Wing loading: 51 kg/m² (10 lb/sq ft)
Power/mass: 0.14 kW/kg (0.09 hp/lb)

Armament

Guns:
1 × forward firing .303 in (7.7 mm) Vickers machine gun
2 × .303 (7.7 mm) Lewis machine gun in flexible mount for observer
Bombs: Up to 500 kg (1,100 lb) of bombs

Aircraft produced by Aero Vodochody

1919-1938	Ae 01 Ae 02 Ae 03 Ae 04 Ae 10 A.11 A.12 A.14 A.15 A.17 A.18 A.19 A.20 A.21 A.22 A.23 A.24 A.25 A.26 A.27 A.29 A.30 A.32 A.34 A.35 A.38 A.42 A.46 A.100 A.101 A.102 A.104 A.125 A.130 A.134 A.200 A.204 A.230 A.300 A.304 A.330 A.430

1945-1992	Ae 45 Ae 50 Ae 145 Ae 245 Ae 345 L-29 L-39 L-59 L-60

1993-present	L-159 Ae 270

Under licence	C-3 C-103 D-44 MB.200

This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.

Aero A.30

Variants

Operators

Specifications (A.230)

See also