About: Lockheed CL-475

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.org associated with source document(s)
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The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology. The CL-475 has a three-bladed main rotor and a two-bladed tail rotor. Only one was built.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:WikicatSingle-enginedPistonHelicopters yago:Aircraft102686568 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Heavier-than-airCraft103510583 yago:Helicopter103512147 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 aircraft yago:Vehicle104524313 yago:Whole100003553 yago:WikicatRigidRotorHelicopters umbel-rc:Model_airplane
rdfs:label	لوكهيد سي إل-475 (ar) Lockheed CL-475 (in) Lockheed CL-475 (en)
rdfs:comment	سي إل-475 (CL-475) طائرة مروحية بمقعد واحد طورتها شركة لوكهيد لاستكشاف امكانيات تكنولوجيا المحركات الدوارة الجامدة. تستخدم محرك أساسي بثلاث مراوح دوارة ومحرك خلفي مثبت على الذيل دوار. بني نموذج واحد منها فقط. (ar) The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology. The CL-475 has a three-bladed main rotor and a two-bladed tail rotor. Only one was built. (en) Lockheed CL-475 (pendaftaran N6940C) adalah helikopter ringan eksperimental dua-kursi, bermesin tunggal, yang dikembangkan oleh Lockheed untuk mengeksplorasi teknologi rotor rigid (kaku). CL-475 memiliki rotor utama berbilah tiga dan rotor ekor berbilah dua. Hanya satu dibangun. (in)
foaf:depiction
dcterms:subject	Single-engined piston helicopters 1950s United States helicopters Rigid rotor helicopters Aircraft first flown in 1959 1950s United States experimental aircraft Lockheed aircraft
Wikipage page ID	23581855 (xsd:integer)
Wikipage revision ID	994144509 (xsd:integer)
Link from a Wikipage to another Wikipage	Rosamond Lake Juan de la Cierva List of rotorcraft Edwards Air Force Base Mojave Desert United States Army Aviation Museum Lockheed Corporation Lockheed XH-51 Lycoming O-360 Single-engined piston helicopters 1950s United States helicopters AH-56 Cheyenne Rigid rotor helicopters Irv Culver Aircraft first flown in 1959 1950s United States experimental aircraft Lockheed aircraft National Air and Space Museum
sameAs	Lockheed CL-475 Lockheed CL-475 Lockheed CL-475 Lockheed CL-475 Lockheed CL-475 Lockheed CL-475 Lockheed CL-475
dbp:wikiPageUsesTemplate	dbt:Lockheed_Martin_aircraft dbt:Cite_book dbt:Commons_category dbt:ISBN dbt:Refbegin dbt:Refend dbt:Reflist dbt:Infobox_aircraft_career dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Lockheed_CL-475.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	1959-11-02 (xsd:date)
national origin	United States (en)
crew	2 (xsd:integer)
designer	Irven Culver (en)
fate	In storage at United States Army Aviation Museum (en)
height ft	9 (xsd:integer)
height in	3 (xsd:integer)
manufacturer	Lockheed Corporation
related	* Lockheed XH-51 (en)
status	Retired (en)
type	Experimental helicopter (en)
civil registration	N6940C (en)
has abstract	سي إل-475 (CL-475) طائرة مروحية بمقعد واحد طورتها شركة لوكهيد لاستكشاف امكانيات تكنولوجيا المحركات الدوارة الجامدة. تستخدم محرك أساسي بثلاث مراوح دوارة ومحرك خلفي مثبت على الذيل دوار. بني نموذج واحد منها فقط. (ar) The Lockheed CL-475 is a two-seat, single-engine light helicopter developed by Lockheed to explore rigid rotor technology. The CL-475 has a three-bladed main rotor and a two-bladed tail rotor. Only one was built. (en) Lockheed CL-475 (pendaftaran N6940C) adalah helikopter ringan eksperimental dua-kursi, bermesin tunggal, yang dikembangkan oleh Lockheed untuk mengeksplorasi teknologi rotor rigid (kaku). CL-475 memiliki rotor utama berbilah tiga dan rotor ekor berbilah dua. Hanya satu dibangun. (in)
ceiling ft	2000 (xsd:integer)
ceiling m	610 (xsd:integer)
empty weight kg	737 (xsd:integer)
empty weight lb	1625 (xsd:integer)
eng1 hp	140 (xsd:integer)
eng1 kw	104 (xsd:integer)
eng1 name	Lycoming VO-360-A1A four-cylinder air-cooled piston engine (en)
eng1 number	1 (xsd:integer)
gross weight kg	907 (xsd:integer)
gross weight lb	2000 (xsd:integer)
height m	2.820000 (xsd:double)
lists	* List of rotorcraft (en)
max speed kmh	145 (xsd:integer)

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