| 词条 | Nord Noroit | |||||||||||||||
| 释义 |
The Nord 1400 Noroit was a French reconnaissance and air-sea rescue flying boat designed and built by Nord Aviation for the French Navy. DevelopmentThe Noroit was an amphibian flying boat designed for the French Navy, a cantilever gullwing monoplane with a two-step hull. It had a cantilever horizontal tail surface with three vertical surfaces. It had an enclosed cabin for the seven crew with a large cabin in the rear for use in rescue operations. The aircraft had two engines located one on each wing leading edge. The prototype as a flying boat first flew on 6 January 1949 powered by two {{convert|1600|hp|kW|abbr=on|disp=flip}} Gnome-Rhône 14R radial engines. The second aircraft was fitted with a retractable tailwheel landing gear for amphibious operation which was later retrofitted to the prototype. The next two aircraft first flown in 1949 were designated the Nord 1401 Noroit and were fitted with two {{convert|1800|hp|kW|abbr=on|disp=flip}} Junkers Jumo 213 engines and both were also tested with two Bristol Hercules radial engines. These two aircraft were modified to production standard as the Nord 1402 Noroit and were followed by 21 production aircraft. The last aircraft was delivered to the French Navy in 1956. Variants
Two prototypes with {{convert|1600|hp|kW|abbr=on|disp=flip}} Gnome-Rhône 14R radial engines.
The first N.1400 Noroit prototype.
The second N.1400 Noroit prototype.
Two pre-production aircraft with {{convert|1800|hp|kW|abbr=on|disp=flip}} Junkers Jumo 213 engines, later modified to 1402 standard.
Production variant, powered by {{convert|2100|hp|kW|abbr=on|disp=flip}} Arsenal 12H engines; 21 built plus two 1401 pre-production aircraft modified. Operators
Specifications (1402){{aerospecs|ref={{cite book |last= |first= |authorlink= |vauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=2617}} |met or eng?=met |crew=seven |capacity= |length m=22.05 |length ft=74 |length in=4 |span m=31.60 |span ft=103 |span in=8 |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=6.85 |height ft=22 |height in=5½ |wing area sqm=100 |wing area sqft=1076.43 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |lift kg= |lift lb= |eng1 number=2 |eng1 type=SNECMA 12H-00 inverted V-12 piston engine |eng1 kw=1566 |eng1 hp=2100 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=370 |max speed mph=230 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=3450 |range miles=2144 |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1=6 x 20mm cannon (two each in nose, dorsal and tail turrets) |armament2=Provision for bombs in engine nacelles |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|see also= |related= |similar aircraft= |sequence= |lists=
}} References{{commons category|Nord Aviation aircraft}}
8 : French military reconnaissance aircraft 1940–1949|Flying boats|Nord aircraft|Gull-wing aircraft|Twin-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1949|Twin-engined piston aircraft |
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