| 词条 | PIK-15 | |||||||||||||||
| 释义 |
The PIK-15 Hinu was a light aircraft developed in Finland in the 1960s for use as a glider tug.[1] It was a low-wing cantilever monoplane of conventional design with an enclosed cockpit and fixed, tailwheel undercarriage.[2] The cockpit had two seats, side-by-side, and the PIK-15 was intended to have a secondary role as a trainer.[1] Construction was of wood throughout.[3] Design work began in 1960, with the first prototype built two years later and flying on 29 August 1964.[2] Six examples were listed on the Finnish Civil Aviation Authority registry in 2011.[4] Specifications (prototype){{aerospecs|ref=Jane's All The World's Aircraft 1965–66[5] |met or eng?=met |crew=One pilot |capacity=1 passenger or instructor |length m=6.60 |length ft=21 |length in=8 |span m=10.00 |span ft=32 |span in=9½ |height m=2.03 |height ft=6 |height in=8 |wing area sqm=14.0 |wing area sqft=150.7 |aspect ratio=7.15:1 |wing profile=NACA 2415 at root, NACA 4409R at tip |empty weight kg=493 |empty weight lb=1,087 |gross weight kg=765 |gross weight lb=1,687 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Lycoming O-320 |eng1 kw=112 |eng1 hp=150 |perfhide=n |max speed kmh=190 |max speed mph=118 |max speed mach= |cruise speed kmh=170 |cruise speed mph=106 |stall speed kmh=90 |stall speed mph=56 |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |g limits= |roll rate= |glide ratio= |climb rate ms=7.0 |climb rate ftmin=1380 }} Notes1. ^1 Taylor 1989, p.726 2. ^1 "PIK-sarjan lentokoneet" 3. ^"PIK-15 HINU '2000+'" 4. ^Summary of the Finnish Aircraft Register 2011, Part I pages 47 and 107 5. ^Taylor 1965, pp. 30–31. References
5 : Finnish special-purpose aircraft 1960–1969|PIK aircraft|Glider tugs|Single-engined tractor aircraft|Low-wing aircraft |
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