OpenLink Software

Usage stats on Lockheed P-80 Shooting Star

 Permalink

an Entity in Data Space: 134.155.108.49:8890

Development of the single engine aircraft began in 1943, based on the British H-1-B-jet engine. The P-80 had an all-metal fuselage design. The first prototype was flown under the callsign XP-80 on 8th January 1944, with a Halford H1 engine (later called the “Goblin”), which was removed from a de Havilland Vampire and sent to the USA, because the first engine was destroyed in an accident. The new aircraft was able to reach a speed of 808 km/h. Because de Havilland was unable to built enough engines for operational P-80 Shooting Stars, the company Allis-Chalmers started building them under license, but this didn't work out. Lockheed then built the Whittle I-40 under license. However, because the new engine was larger than the H-1 engine, the fuselage of the P-80 had be enlarged as well.

Graph IRICount
http://dbkwik.webdatacommons.org16
Alternative Linked Data Views: ODE     Raw Data in: CXML | CSV | RDF ( N-Triples N3/Turtle JSON XML ) | OData ( Atom JSON ) | Microdata ( JSON HTML) | JSON-LD    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] This material is Open Knowledge Creative Commons License Valid XHTML + RDFa
This work is licensed under a Creative Commons Attribution-Share Alike 3.0 Unported License.
OpenLink Virtuoso version 07.20.3217, on Linux (x86_64-pc-linux-gnu), Standard Edition
Copyright © 2009-2012 OpenLink Software