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May also have been designated J-6 Xin. [1] Another name is "J-6III". The name D-type was coined as a piggyback. Shenyang/Tianjin JJ-6 – (Jianjiji Jiaolianji – fighter trainer, a.k.a. Product 48 and FT-6) Chinese designed two-seat trainer, stretched 84 cm (33.1 in) to accommodate second seat, armed with one 30 mm cannon. [1]
J-7II target towing jet: J-7II converted for target towing, with belly tank replaced by Type Aerial Drone (空靶) 4 aerial drone for antiaircraft guns or aircraft gunnery practice. [ 23 ] [ 25 ] J-7IIS : Stealth research aircraft (serial # 137) used to explore measures to reduce radar cross section without changing the shape of the existing ...
A jointer cannot be used to create a board of even thickness along its length. For this task, after jointing one face, a thickness planer is used. Thickness planers and jointers are often combined into one machine, with the work piece passing underneath the same rotating blade for thicknessing, but in the opposite direction.
(Dr Lewis A Jackson, Central State Univ, Wilberforce, OH) Jackson Versatile I N9666H, tractor propeller, folding parasol wing [3] [7] [8]; Jackson N8072 1956, pusher propeller, low-wing monoplane with folding wings, experimental, roadable aircraft [9]
The Chinese jet also passed the nose of the P-8 at 90 degrees with its belly toward the P-8 Poseidon, believed to be displaying its weapons load-out. Afterwards, the J-11 flew directly under and alongside the P-8, bringing their wingtips, as I said, to within 20 feet [6 m]. And then conducted a roll over the P-8, passing within 45 feet [14 m]."
One thing to note is that the Nanchang CJ-6 makes extensive use of pneumatics to control the gear and flap extension/retraction, operate the brakes and start the engine. An engine-driven air pump recharges the system; however if air pressure is too low to start the engine then the onboard air tank can be recharged by an external source.
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The J-9B-VI was a canard-delta with lateral intakes; a single ventral intake was rejected. The intended engine, the Woshan WS-6 turbofan, encountered development problems; a reverse-engineered Khachaturov R29-300 turbojet, to be called the WS-15, was selected as a less powerful alternative. [2]
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