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Dornier Aerodyne

The Dornier Aerodyne[1] (also referred to as "Lippisch-Dornier Aerodyne"[2]) was a wingless VTOL unmanned aircraft. Conceived by Alexander Lippisch, it was developed and built by Dornier on behalf of the Federal German Ministry of Defence (BMVg). Lippisch was part of the team.[2] The first flight took place on 18 September 1972. The development ended on 30 November 1972 after successful hovering-flight testing with the aircraft. Experimentation did not continue due to lack of interest by the Bundeswehr (German Armed Forces).[citation needed]

Aerodyne
The Aerodyne on display at the Deutsches Museum Flugwerft Schleissheim[1]
Role VTOL Experimental aircraft
National origin West Germany
Manufacturer Dornier Flugzeugwerke
Designer Alexander Lippisch
First flight 18 September 1972
Retired 30 November 1972
Primary user Federal German Ministry of Defence
Number built 1

Description Edit

The principle behind the Aerodyne is the combination of lift and thrust production in a single construction unit and flow channel, i.e. a ducted fan. Flaps at the end of the fan divert the outflowing air to produce lift, thrust, or a combination of both. As a result, the Aerodyne could be steered and flown in the entire range between hovering and full-forward flight.

For forward flight, the Aerodyne had a conventional tail unit at the rear, which allowed for pitch and yaw control. The equipment was unmanned and operated by remote control.

It was intended to be a land- or ship-supported drone (UAV) for aerial reconnaissance.

Specifications Edit

  • Length: 5.5 metres (18 ft)
  • Width: 1.9 metres (6 ft 3 in)
  • Fan Diameter: 1.1 metres (3 ft 7 in)
  • Engine: 1 MTU 6022 A-3, 370 shaft horsepower (280 kW)
  • Total Weight: 435 kilograms (959 lb)

References Edit

  1. ^ a b Deutsches Museum: Aerodyne, retrieved 19 March 2021.
  2. ^ a b KRISTINA KIRKLIAUSKAITE, "Lippisch-Dornier Aerodyne: Wingless and tailless aircraft", Aerotime, retrieved 19 March 2021.

"Eine Dokumentation zur Geschichte des Hauses Dornier", Ed. Dornier GmbH, 1983, bound, 214 pp.

  • Patents US2918230; US2918233.

dornier, aerodyne, this, article, multiple, issues, please, help, improve, discuss, these, issues, talk, page, learn, when, remove, these, template, messages, this, article, needs, additional, citations, verification, please, help, improve, this, article, addi. This article has multiple issues Please help improve it or discuss these issues on the talk page Learn how and when to remove these template messages This article needs additional citations for verification Please help improve this article by adding citations to reliable sources Unsourced material may be challenged and removed Find sources Dornier Aerodyne news newspapers books scholar JSTOR August 2008 Learn how and when to remove this template message This article includes a list of general references but it lacks sufficient corresponding inline citations Please help to improve this article by introducing more precise citations August 2008 Learn how and when to remove this template message Learn how and when to remove this template message The Dornier Aerodyne 1 also referred to as Lippisch Dornier Aerodyne 2 was a wingless VTOL unmanned aircraft Conceived by Alexander Lippisch it was developed and built by Dornier on behalf of the Federal German Ministry of Defence BMVg Lippisch was part of the team 2 The first flight took place on 18 September 1972 The development ended on 30 November 1972 after successful hovering flight testing with the aircraft Experimentation did not continue due to lack of interest by the Bundeswehr German Armed Forces citation needed AerodyneThe Aerodyne on display at the Deutsches Museum Flugwerft Schleissheim 1 Role VTOL Experimental aircraftNational origin West GermanyManufacturer Dornier FlugzeugwerkeDesigner Alexander LippischFirst flight 18 September 1972Retired 30 November 1972Primary user Federal German Ministry of DefenceNumber built 1Description EditThe principle behind the Aerodyne is the combination of lift and thrust production in a single construction unit and flow channel i e a ducted fan Flaps at the end of the fan divert the outflowing air to produce lift thrust or a combination of both As a result the Aerodyne could be steered and flown in the entire range between hovering and full forward flight For forward flight the Aerodyne had a conventional tail unit at the rear which allowed for pitch and yaw control The equipment was unmanned and operated by remote control It was intended to be a land or ship supported drone UAV for aerial reconnaissance Specifications EditLength 5 5 metres 18 ft Width 1 9 metres 6 ft 3 in Fan Diameter 1 1 metres 3 ft 7 in Engine 1 MTU 6022 A 3 370 shaft horsepower 280 kW Total Weight 435 kilograms 959 lb References Edit a b Deutsches Museum Aerodyne retrieved 19 March 2021 a b KRISTINA KIRKLIAUSKAITE Lippisch Dornier Aerodyne Wingless and tailless aircraft Aerotime retrieved 19 March 2021 Eine Dokumentation zur Geschichte des Hauses Dornier Ed Dornier GmbH 1983 bound 214 pp Patents US2918230 US2918233 Retrieved from https en wikipedia org w index php title Dornier Aerodyne amp oldid 1100644343, wikipedia, wiki, book, books, library,

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