词条 | Thaden T-2 | |||||||||||||||
释义 |
The Thaden T-2 was a 1920s American four-seat all-metal cabin monoplane built by the Thaden Metal Aircraft Company of San Francisco, California. Design and developmentThe Thaden Metal Aircraft Company was formed by Herbert von Thaden, a former United States Army Signal Corps pilot and engineer to work on developing the first American all-metal aircraft. Following on from the strut-braced T-1 the T-2 was a smaller four-seat high-wing cantilever monoplane with flaps and powered by a {{convert|150|hp|kW|0|abbr=on}} Comet radial engine. Specifications{{aerospecs|ref=www.aerofiles.com |met or eng?=met |genhide= |crew= |capacity=4 |length m=7.65 |length ft=25 |length in=1 |span m=11.89 |span ft=39 |span in=0 |height m= |height ft= |height in= |wing area sqm= |wing area sqft= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=1 |eng1 type=Comet 7-D air-cooled radial piston engine |eng1 kw=112 |eng1 hp=150 |eng2 number= |eng2 type= |perfhide= |max speed kmh=194 |max speed mph=121 |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= }} See also{{Portal|Aviation}}
References{{commons category|Thaden aircraft}}
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5 : United States civil utility aircraft 1920–1929|Economy of San Francisco|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1928 |
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