Dornier Do 29
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Original source: Own work Author Martin.bergner [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue
Author: Martin.bergner [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue

The Dornier Do 29 was an experimental aircraft developed by Dornier Flugzeugwerke and the Deutsche Versuchsanstalt für Luftfahrt (German Aviation Laboratory) in the 1950s used to test a tilting-propeller system for short takeoff and landing aircraft. The concept was proved to be successful in flight testing however no further development of the system or aircraft was proceeded with and at the conclusion of its test program the Do 29 was retired.

Die Dornier Do 29 war ein Erprobungsträger auf Basis der Do 27. Die YA+101 war einige Jahre in der Koblenzer Wehrtechnischen Studiensammlung ausgestellt, bevor sie hier ins Lager gekommen ist.1
Dornier Do 29 mit um bis zu 90° nach unten schwenkbaren Druckpropellern ausgerüstet.2

Made by Dornier Flugzeugwerke.

It is the successor of the Dornier Do 27 .

Il Dornier Do 29 fu un velivolo sperimentale, sviluppato da Dornier-Werke e da Deutsches Zentrum für Luft- und Raumfahrt (agenzia tedesca che si occupa della ricerca e sperimentazione in campo aeronautico) negli anni '50, con il quale si voleva sperimentare il decollo e atterraggio breve (STOL) grazie all'inclinazione delle eliche.3
Wing Area Sqm
22
Predecessor
Dornier Do 27
Eng 1 Type
geared opposed piston engines
Lists
* List of experimental aircraft* List of military aircraft of Germany
Range Km
400
Max Speed Kmh
290
Developed From
Dornier Do 27
Gross Weight Lb
5291
Similar Aircraft
* Ryan VZ-3
Crew
1
Prop Blade Number
3
Height In
10
Primary user
Max Takeoff Weight Kg
2500
Manufacturer
First Flight
12
Eng 1 Name
Lycoming GO-480-B1A6
Production End Year
0002
Height Ft
8
Origin
Germany
National Origin
Germany
Production Start Year
0002
Minimum Control Speed Kmh
24
Span M
13
Prime Units
met
Ceiling M
6500
Eng 1 Hp
270
Eng 1 Number
2
Produced
2
Length M
10
Category

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