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Gotha Go 242

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Transport glider used by the Luftwaffe during World War II

Gotha Go 242
Gotha Go 242 inGrosseto, 1943
General information
TypeTransport glider
ManufacturerGothaer Waggonfabrik
Designer
Albert Kalkert
Primary userLuftwaffe
Number built1,528[1]
History
Introduction date1941
First flight1941

TheGotha Go 242 was atransport glider used by theLuftwaffe duringWorld War II. It was an upgrade over theDFS 230 in both cargo/troop capacity and flight characteristics. It saw limited combat action. There were multiple glider variants, and it became the basis for a transport aircraft, the:Gotha Go 244.

Development

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The Go 242 was designed by Dipl-Ing Albert Kalkert in response to aReichsluftfahrtministerium (RLM) requirement for a heavy transport glider to replace theDFS 230 then in service. The requirement was for a glider capable of carrying 20 fully laden troops or the equivalent cargo.

The aircraft was a high-wingmonoplane with a simple square-sectionfuselage ending in clamshell doors used to load cargo.[2] The empennage was mounted on twin booms linked by a tailplane. The fuselage was formed of steel tubing covered withdoped fabric. The flight characteristics of the design were better than those of the DFS 230.

Cargo versions of the glider featured a hinged rear fuselage loading ramp that could accommodate a small vehicle such as aKübelwagen or loads of similar size and weight.[2]

Two prototypes flew in1941 and the type quickly entered production. A total of 1,528 were built, 133 B-1 to B-5s were converted[1] to theGo 244, with two 500 kW (670 hp)Gnome-Rhône 14M engines, (a paired -04 and -05 rotating in opposite directions), fitted to forward extensions of the tail booms.

The Go 242 was tested with various rockets for overloaded take offs. A rack of four 470 N (106 lbf) Rheinmetall-Borsig 109-502 rockets mounted on the rear of the cargo compartment was tested but not used operationally. A second rocket, called "R-Gerät", also used with the glider, was a liquid-fuelledWalter HWK 109-500A (R I-203)Starthilfe; a podded monopropellant (T-Stoff, stabilised high test peroxide), rocket engine mounted beneath each wing and jettisoned after take-off, parachuting down to be recycled.

Operational history

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German troops seated in a Go 242, Russia, 1943. The glider is fitted with defensive machine guns

In service, Go 242s were towed into the air byHeinkel He 111s orJunkers Ju 52s, and were occasionally fitted withRATO equipment. Most saw service in theMediterranean,North Africa andAegean.Ju 87D-2s had strengthened rear fuselage and combined tailwheel and hook for towing the Go 242.[citation needed]

A few gliders, the Go 242 C-1 variant, were constructed with aflying boat-style hull allowing water landings. It was proposed that some carry a smallcatamaran assault boat with a 1,200 kg (2,600 lb) explosive charge suspended between its hulls. The proposed mission profile was for the pilot to land near an enemy ship and transfer to the assault boat, setting off at high speed for the enemy ship and locking the controls before bailing out.[3][2]

Surviving aircraft

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Variants

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  • Go 242 A-1 - initial cargo-carrying version
  • Go 242 A-2 - initial troop-carrying version
  • Go 242 B-1 - cargo version with jettisonable landing gear
  • Go 242 B-2 - B-1 with improved landing gear
  • Go 242 B-3 - troop-carrying version of B-1 with double rear doors
  • Go 242 B-4 - troop-carrying version with doors of B-3 and landing gear of B-2
  • Go 242 B-5 - training version with dual controls
  • Go 242 C-1 - maritime assault version withflying boat-style hull. Never used operationally

Specifications (Go 242B)

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Data from Die Deutsche Luftruestung 1933–1945 Vol.2 – Flugzeugtypen Erla-Heinkel[4]

General characteristics

  • Crew: 2
  • Capacity: 23 equipped troops or 3,500–4,000 kg (7,700–8,800 lb) cargo
  • Length: 15.8 m (51 ft 10 in)
  • Wingspan: 24.5 m (80 ft 5 in)
  • Height: 4.7 m (15 ft 5 in)
  • Wing area: 64.4 m2 (693 sq ft)
  • Aspect ratio: 9.32
  • Empty weight: 3,200 kg (7,055 lb)
  • Max takeoff weight: 7,100 kg (15,653 lb)

Performance

  • Never exceed speed: 300 km/h (190 mph, 160 kn)
  • Maximum glide ratio: 16:1
  • Towing speed: 240 km/h (150 mph; 130 kn)

Armament

  • 4 × 7.92 mm (0.312 in)MG 15 machine-guns

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

Notes

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  1. ^abMunson 1978, p. 69.
  2. ^abcFord, Roger (2013).Germany's Secret Weapons of World War II. London, United Kingdom: Amber Books. p. 224.ISBN 9781909160569.
  3. ^Wood, Paul; Roger Ford (2000).Germany's secret weapons in World War II. Zenith Imprint.ISBN 0-7603-0847-0.
  4. ^Nowarra, Heinz J. (1993).Die Deutsche Luftruestung 1933–1945 Vol.2 – Flugzeugtypen Erla-Heinkel (in German). Koblenz: Bernard & Graefe Verlag. pp. 139–142,268–269.ISBN 3-7637-5464-4.

Further reading

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  • Metzmacher, Andreas (2021).Gotha Aircraft 1913-1954: From the London Bomber to the Flying Wing Jet Fighter. Brimscombe, Stroud: Fonthill.ISBN 978-1-78155-706-8.
  • Munson, Kenneth (1978).German Aircraft Of World War 2 in colour. Poole, Dorsett, UK: Blandford Press.ISBN 0-7137-0860-3.
  • Nowarra, Heinz; Force, Ed (1991).German Gliders in World War II. Atglen, Pennsylvania: Schiffer Publishing.ISBN 0-88740-358-1.

External links

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Wikimedia Commons has media related toGotha Go 242.
Gotha aircraft
Company designations pre-1918
Idflieg designations 1914-1918
RLM designations 1933-1945
Project numbers
1 to 100
101 to 200
201 to 300
301 to 349
Post-349 (non-sequential)
  • 1 Not assigned
  • 2 Unofficial/proposed
  • 3 Assigned, but not used before RLM was dissolved
  • 4 Assigned to captured aircraft
  • 5 Unconfirmed
  • 6 Propaganda/cover designation
  • 7 Assigned to multiple types

Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

Authority control databases: NationalEdit this at Wikidata
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