| 词条 | Paumier MP2 Baladin | |||||||||||||||
| 释义 |
The Paumier MP2 Baladin is a French-built light sporting aircraft of the 1960s.
Design and constructionThe MP2 Baladin was designed and constructed by Maurice Paumier. The two-seat side-by-side design was advanced for its day amongst amateur constructors, as it featured such refinements as a variable-pitch airscrew, landing flaps and a retractable tricycle undercarriage. The aircraft possessed an exceptionally clean finish, being of wooden construction with plywood- and fabric-covered wings and a plywood-covered fuselage. These features enabled the Baladin to attain a maximum speed of 158 mph on a 90 h.p. engine. A one-piece all-moving tailplane is employed, and a feature of the design is the large wingtip endplate which slides rearward for access to the fuel filler pipe.[1] Operational historyThe prototype MP2 Baladin F-PJKV has had a series of private owners since its first flight in early 1961. It is currently (early 2009) operational from its base at Beauvais-Tille airport near Paris. A second example F-PPPC was built and initially based at Guyancourt aerodrome near Paris. Specifications(per Green, 1965, p. 59) {{aerospecs|ref= |met or eng?=met |crew=1 |capacity=1 passenger |length m=5.95 |length ft=19 |length in=6 |span m=7.60 |span ft=24 |span in=11 |swept m= |swept ft= |swept in= |rot number= |rot dia m= |rot dia ft= |rot dia in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m=2.60 |height ft=8 |height in=6 |wing area sqm=9.80 |wing area sqft=105.5 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |wing profile= |empty weight kg=375 |empty weight lb=827 |gross weight kg=615 |gross weight lb=1,356 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Continental C90 four cylinder air-cooled |eng1 kw=67 |eng1 hp=90 |max speed kmh=255 |max speed mph=158 |max speed mach= |cruise speed kmh=228 |cruise speed mph=142 |stall speed kmh= |stall speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |g limits= |roll rate= |glide ratio= |climb rate ms=4.8 |climb rate ftmin=945 |sink rate ms= |sink rate ftmin= }} References
1. ^Green, 1965, p. 59 {{refbegin}}
4 : French civil utility aircraft 1960–1969|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1961 |
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