|
“ú‰pƒeƒNƒjƒJƒ‹Eƒf[ƒ^ TECHNICAL SPECIFICATION ¦“ú‰pƒeƒNƒjƒJƒ‹Eƒf[ƒ^‚ÉŠÖ‚µ‚Ă̂²Ž¿–â‚Ínakamura@skynet-1.com‚Ü‚ÅB |
|
‹@‘̔Ԇ DESIGNATION §Ž®–¼Ì TYPE NUMBER ’ÊÌ NICKNAME ÝŒv DESIGN AND MANUFACTURER ‹@Ží—p“r DUTY Œ^Ž® TYPE ‰†Š®¬ PROTOTYPE ¶ŽY PRODUCTION QUANTITY æˆõ CREW ”“®‹@ ENGINE –¼Ì MODEL Œ^Ž® TYPE AND CYLINDERS Šî” NUMBER ’¼Œa DIAMETER ‘S’· LENGTH d—Ê WEIGHT —£¸o—Í TAKE OFF POWER ŒöÌo—Í NORMAL POWER 퓬o—Í MILITARY POWER ƒvƒƒyƒ‰ PROPELLER –¼ÌŒ^Ž® MODEL AND TYPE ãÀ” NUMBERS OF BLADE ’¼Œa DIAMETER ƒsƒbƒ` PITCH SETTING d—Ê WEIGHT ‘S‘Ì GENERAL ‘S• SPAN ‘S’· OVER ALL LENGTH ‘S‚ OVER ALL HEIGHT …•½ HORIZONTAL ATTITUDE ‚R“_ TAIL DOWN Žå—ƒ WING ‘S• SPAN –ÊÏ AREA •tªŒ·’· CHORD AT ROOT —ƒ’[Œ·’· CHORD AT TIP Œã‘ÞŠp SWEPT ANGLE 㔽Šp DIHEDRAL Žæ•tŠp INCIDENCE €‚艺‚° TWIST DOWN c‰¡”ä ASPECT-RATIO ‹ó—Í“I•½‹Ï—ƒŒ· M. A. C.iMEAN AERODYNAMIC CHORDj —ƒ’f–Ê AIRFOIL SECTION •â•—ƒ AILERON • SPAN •tªŒ·’· CHORD AT ROOT —ƒ’[Œ·’· CHORD AT TIP –ÊÏ AREA ì“®Šp RANGE OF MOVEMENT ƒtƒ‰ƒbƒv FLAP ő匷’· MAX. CHORD –ÊÏ AREA Å‘åŠJŠp“x MAX. MOVEMENT …•½”ö—ƒ HORIZONTAL STABILIZER • SPAN ő匷’· MAX. CHORD ˆÀ’è”–ÊÏ STABILIZER AREA ¸~‘Ç–ÊÏ ELEVATOR AREA Œv TOTAL AREA Žæ•tˆÊ’u SETTING POSITION Žæ•tŠp INCIDENCE ì“®Šp RANGE OF MOVEMENT@@@ã@UP@‰º@DOWN ‚’¼”ö—ƒ FINCVERTICAL STABILIZER ‚‚³ HEIGHT ő匷’· MAX. CHORD ˆÀ’è”–ÊÏ VERTICAL STABILIZER AREA •ûŒü‘Ç–ÊÏ RUDDER AREA Œv TOTAL AREA Žæ•tŠp SETTING ANGLE ì“®Šp MOVEMENT@@@¶@LEFT@‰E@RIGHT “·‘Ì FUSELAGE ‘S’· OVER ALL LENGTH Å‘å‚ MAX. HEIGHT Å‘å• MAX. WIDTH ~’…‘•’u LANDING GEAR ŽÔ—ÖŠÔŠu WHEEL TRACKiTREADj ŽÔ޲ŠÔŠu WHEEL BASE ŽåŽÔ —Ö MAIN WHEEL ”ö—Ö TAIL WHEEL ‚R“_ÃŽ~Šp THREE POINT ANGLE STATIC LOADED •‘• ARMAMENT ‹@e GUNS ”š’e BOMBS –³ü RADIO ”R—¿ FUEL ƒ^ƒ“ƒN FUEL TANK CAPACITIES ŠŠ–û OIL ƒ^ƒ“ƒN OIL TANK CAPACITIES d—Ê WEIGHT Ž©d BASIC WEIGHT ‘S”õd—Ê GROSS WEIGHT ‰ß‰×d—Ê OVER LOAD WEIGHT ő嗣—¤ MAX. TAKE-OFF WEIGHT ”ä RATIO —ƒ–ʉ×d WING LOADING ”n—͉×d POWER LOADING «”\ PERFORMANCE ő呬“x MAX. SPEED „q‘¬“x CRUISING SPEED ’…—¤‘¬“x LANDING SPEED 㸎žŠÔ CLIMB TIME ŽÀ—p㸌À“x SERVICE CEILING q‘±‹——£ RANGE |