About: Dornier Do 29

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

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.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Dornier Do 29
rdfs:comment	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.
sameAs	dbr:Dornier_Do_29
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dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/ODD2urn6xOTu5tfNx3dKHA== dbkwik:resource/ZbtrzLFw6TNwE1208cbZTA== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/CtbfVERA8rrkkb3qmAFx5A== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/sgy-37hYEWSi0ff69o00Qg== dbkwik:resource/53QMiWPdneI2OH9P4UqvyQ== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw== dbkwik:resource/uhdoHROSoHPwlMhaO_LDdA==
prop blade number	3(xsd:integer)
range km	400(xsd:integer)
Produced	2(xsd:integer)
eng1 type	geared opposed piston engines
primary user	dbkwik:resource/UMD_ozeBMPSoAQiNRM3Z3A==
Type	Experimental aircraft
Height in	10(xsd:integer)
span m	13(xsd:double)
Manufacturer	Dornier Flugzeugwerke
max speed kmh	290(xsd:integer)
minimum control speed kmh	24(xsd:integer)
ceiling m	6500(xsd:integer)
length m	9(xsd:double)
National Origin	Germany
Developed From	Dornier Do 27
Height ft	8(xsd:integer)
First Flight	1958-12-12(xsd:date)
gross weight lb	5291(xsd:integer)
max takeoff weight kg	2500(xsd:integer)
wing area sqm	21(xsd:double)
prime units?	met
Crew	1(xsd:integer)
eng1 name	Lycoming GO-480-B1A6
eng1 hp	270(xsd:integer)
eng1 number	2(xsd:integer)
abstract	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.
is Developed Into of	Dornier Do 27

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