DFS 230F

DFS 230F
Role Assault glider
National origin Germany
Manufacturer Gothaer Waggonfabrik
Designer Ing. Hünerjäger[1]
First flight late 1943[1]
Number built 1[1]

The DFS 230 V7 / DFS 230F was an assault glider designed and built in Germany during 1943 that was only built in prototype form.[1]

Design and development

The RLM (Reichsluftfahrtministerium - German Air Ministry), issued a directive in 1941 that no effort was to be spent designing a replacement for the rather dated DFS 230 assault glider, in its weight class. Ing. Hünerjäger of Gothaer Waggonfabrik (Gotha) believed that a great improvement on the DFS 230 could be achieved with an aircraft of similar dimensions designing what was named the DFS 230 V7 despite the ban. Gotha named their new design's prototype DFS 230 V7, production aircraft were to be designated DFS 230F-1, to deflect criticism for ignoring the ban on DFS 230 replacement.[1]

Completed in 1943 the DFS 230 V7 had a cargo hold measuring 4.5 m (15 ft) x 1.5 m (5 ft) x 1.5 m (5 ft), a vast improvement on the DFS 230. Access to the hold was via large hatches in the fuselage sides and roof of the rear fuselage. For assault glider missions a crew of two would fly the aircraft with up to 11 Fallschirmjäger or up to 1,750 kg (3,858 lb) of cargo in overload conditions.[1]

Despite successful flight trials no orders for production aircraft were forthcoming and only the prototype was built.[1]

Variants

Data from:'[1]

(Gotha) DFS 230 V7
The prototype of an assault glider in the same class as the DFS 230 (an altogether new design)
(Gotha) DFS 230F-1
The proposed production version

Specifications (DFS 230 V7)

Data from Aircraft of the Third Reich[1]

General characteristics

  • Crew: 2
  • Capacity: 11 Fallschirmjäger or up to 1,750 kg (3,858 lb) of cargo in overload conditions.
  • Length: 12.5 m (41 ft 0 in)
  • Wingspan: 19.4 m (63 ft 8 in)
  • Height: 2.9 m (9 ft 6 in)
  • Wing area: 39.5 m2 (425 sq ft)
  • Empty weight: 1,253 kg (2,762 lb)
  • Gross weight: 2,400 kg (5,291 lb)
  • Max takeoff weight: 3,000 kg (6,614 lb)

Performance

  • Never exceed speed: 330 km/h (205 mph; 178 kn)
  • Maximum towing speed: 300 km/h (186 mph)
  • Landing speed: 95 km/h (59 mph)

See also

Aircraft of comparable role, configuration and era

References

  1. 1 2 3 4 5 6 7 8 9 Green, William (2010). Aircraft of the Third Reich (1st ed.). London: Aerospace Publishing Limited. p. 194. ISBN 978-1-900732-06-2.
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