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Lippisch Delta IV

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1936 experimental aircraft
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DFS 39
General information
TypeExperimental
ManufacturerDeutsche Forschungsanstalt für Segelflug
Designer
Number built1
History
First flight1936
Developed fromFieseler F 3
VariantDFS 40

Alexander Lippisch'sDelta IV was a continuation of his work ondelta wing designs pioneered in hisDelta I,Delta II andDelta III aircraft.

Design and development

[edit]

Fieseler F 3Wespe

[edit]

The project began with an order fromGerhard Fieseler for a design thathis company could build for him to fly in the 1932Europarundflug air rally. The result was a highly unorthodox design, sporting large delta wings,canards, and an engine and propeller mounted in both the nose and tail of the plane.

Fieseler built this design as theF 3Wespe ("Wasp"), but it proved highly unstable, causing Fieseler to crash it on his first flight. Further refinements were unable to correct these deficiencies, and after one final crash, Fieseler abandoned the aircraft.

DFS 39

[edit]

Lippisch continued to believe that the problems were surmountable, and found an ally in ProfessorWalter Georgii of the DFS (Deutsche Forschungsanstalt für Segelflug – German Research Institute for Sailplane Flight). Georgii secured funding from the RLM (Reichsluftfahrtministerium – Reich Air Ministry) to purchase the aircraft from Fieseler and work on perfecting it. At the DFS, Lippisch rebuilt the aircraft, removing the canards and the rear engine and renaming it theDelta IVa.

Although this flew much better than its predecessor, it was still involved in a very serious crash which led to an investigation of Lippisch's endeavours. The RLM and the DVL (Deutsche Versuchsanstalt für Luftfahrt – German Aviation Research Institute) eventually concluded that the Delta series was not only dangerous, but an aeronautical dead end. Only Georgii's continued support prevented them from ordering the discontinuation of the research.

The aircraft was rebuilt again, this time incorporating new aerodynamic refinements based on Lippisch's experiences with his recentStorch Xglider. The new incarnation, dubbedDelta IVb proved to be a step in the right direction.

Success finally came with a last round of changes. The aircraft was rebuilt yet again, making the sweep of its wings less severe, and adding small, downturned fins at their tips. The fuselage was lengthened somewhat, and a small rudder was added to it. Now called theDelta IVc, the result was finally what Lippisch had been looking for. In 1936, the aircraft was taken to theLuftwaffe flight-testing centre atRechlin where test pilotHeini Dittmar put it through its paces, gaining an airworthiness certificate for the type and an official RLM designation –DFS 39.

Messerschmitt Me 163

[edit]

It proved to be an extremely stable and well-behaved design, and now attracted the interest of the RLM as the basis for arocket-powered research aircraft. The work was kept secret and the new variant of the Delta IV referred to asProject X. The airframe was to make significant use of metal construction, which was not available at the DFS, so Lippisch andProjekt X were transferred toMesserschmitt. It was redesignated the Me 163 and would eventually appear as theMesserschmitt Me 163 Komet rocket fighter.[1]

Specifications (DFS 39d)

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Lippisch DFS 39, 1936

Data fromDie Deutsche Luftrüstung 1933–1945 Vol.1 – AEG-Dornier[2]

General characteristics

  • Crew: 2
  • Length: 5.4 m (17 ft 9 in)
  • Wingspan: 9.6 m (31 ft 6 in)
  • Height: 1.8 m (5 ft 11 in)
  • Wing area: 13.4 m2 (144 sq ft)
  • Empty weight: 390 kg (860 lb)
  • Max takeoff weight: 600 kg (1,323 lb)
  • Fuel capacity: 150 L (40 US gal; 33 imp gal) fuel; 16 L (4.2 US gal; 3.5 imp gal) oil
  • Powerplant: 1 ×Pobjoy R 7-cylinder air-cooled geared radial piston engine 85 PS (84 hp; 63 kW)
  • Propellers: 2-bladed wooden fixed-pitch propeller, 2.1 m (6 ft 11 in) diameter

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn) at sea level
  • Cruise speed: 180 km/h (110 mph, 97 kn)
  • Landing speed:70 km/h (43 mph; 38 kn)
  • Range: 1,350 km (840 mi, 730 nmi)
  • Service ceiling: 6,300 m (20,700 ft)
  • Rate of climb: 5.8 m/s (1,140 ft/min)
  • Time to altitude: 1,000 m (3,300 ft) in 3 minutes

References

[edit]
  1. ^ Lippisch, Alexander M. "Tailless Tailpiece".Air Enthusiast. September 1972. pp.136-8, 150.
  2. ^Nowarra, Heinz J. (1993).Die Deutsche Luftrüstung 1933–1945 Vol.1 – AEG-Dornier (in German). Koblenz: Bernard & Graefe Verlag. pp. 159–160,244–245.ISBN 978-3-7637-5464-9.

External links

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Wikimedia Commons has media related toLippisch aircraft.
Wikimedia Commons has media related toFieseler F 3 Wespe.
DFS Names
RLM designations
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.

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