Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q7388617> ?p ?o }
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- Q7388617 subject Q7464706.
- Q7388617 subject Q8387110.
- Q7388617 subject Q9411434.
- Q7388617 abstract "The Lark project was a high-priority, solid-fuel boosted, liquid-fueled rocket surface-to-air missile developed by the United States Navy to meet the kamikaze threat. After Lark configuration was established by the Bureau of Aeronautics in January 1945 Fairchild Aircraft was given a contract to produce 100 missiles in March 1945. Fairchild used radio command guidance with a semi-active radar homing AN/DPN-7. A backup contract for another 100 missiles was given to Convair in June 1945. Convair used beam riding guidance with AN/APN-23 active radar homing. Neither version was successful. Six of the Convair airframes were given to Raytheon to explore use of velocity-gated continuous wave doppler radar for guided missile target seekers, while most other United States investigators used range-gated pulse radar. One of these Raytheon guidance systems in a Convair airframe scored the first successful United States surface-to-air missile interception of a flying target in January 1950.".
- Q7388617 diameter "0.4572".
- Q7388617 length "5.4864".
- Q7388617 origin Q30.
- Q7388617 thumbnail PointMuguLark.jpg?width=300.
- Q7388617 type Q466704.
- Q7388617 weight "920000.0".
- Q7388617 wikiPageWikiLink Q1029234.
- Q7388617 wikiPageWikiLink Q11220.
- Q7388617 wikiPageWikiLink Q11223.
- Q7388617 wikiPageWikiLink Q1133809.
- Q7388617 wikiPageWikiLink Q1136766.
- Q7388617 wikiPageWikiLink Q1143706.
- Q7388617 wikiPageWikiLink Q1187984.
- Q7388617 wikiPageWikiLink Q1190906.
- Q7388617 wikiPageWikiLink Q133194.
- Q7388617 wikiPageWikiLink Q1334213.
- Q7388617 wikiPageWikiLink Q156644.
- Q7388617 wikiPageWikiLink Q1785862.
- Q7388617 wikiPageWikiLink Q1972210.
- Q7388617 wikiPageWikiLink Q243249.
- Q7388617 wikiPageWikiLink Q2906424.
- Q7388617 wikiPageWikiLink Q293810.
- Q7388617 wikiPageWikiLink Q30.
- Q7388617 wikiPageWikiLink Q3268417.
- Q7388617 wikiPageWikiLink Q333133.
- Q7388617 wikiPageWikiLink Q3647257.
- Q7388617 wikiPageWikiLink Q4052260.
- Q7388617 wikiPageWikiLink Q4335256.
- Q7388617 wikiPageWikiLink Q466704.
- Q7388617 wikiPageWikiLink Q47528.
- Q7388617 wikiPageWikiLink Q741745.
- Q7388617 wikiPageWikiLink Q7464706.
- Q7388617 wikiPageWikiLink Q836947.
- Q7388617 wikiPageWikiLink Q8387110.
- Q7388617 wikiPageWikiLink Q9212.
- Q7388617 wikiPageWikiLink Q9411434.
- Q7388617 length "18.0".
- Q7388617 length "booster:".
- Q7388617 length "missile:".
- Q7388617 name "Lark".
- Q7388617 origin Q30.
- Q7388617 type Q466704.
- Q7388617 weight "920.0".
- Q7388617 weight "booster:".
- Q7388617 weight "missile:".
- Q7388617 type Product.
- Q7388617 type Device.
- Q7388617 type Weapon.
- Q7388617 type Thing.
- Q7388617 type Q728.
- Q7388617 comment "The Lark project was a high-priority, solid-fuel boosted, liquid-fueled rocket surface-to-air missile developed by the United States Navy to meet the kamikaze threat. After Lark configuration was established by the Bureau of Aeronautics in January 1945 Fairchild Aircraft was given a contract to produce 100 missiles in March 1945. Fairchild used radio command guidance with a semi-active radar homing AN/DPN-7. A backup contract for another 100 missiles was given to Convair in June 1945.".
- Q7388617 label "SAM-N-2 Lark".
- Q7388617 depiction PointMuguLark.jpg.
- Q7388617 name "Lark".