| 词条 | Dalotel DM-165 | |||||||||||||||
| 释义 |
The Dalotel DM-165 was a French two-seat training monoplane designed by Michel Dalotel.[1] A number of variants were proposed but only the prototype was built.[1] Design and developmentThe DM-165 was a tandem two-seat low-wing monoplane. Powered by a 165 hp (121 kW) Continental IO-346A flat-four piston engine. It had a tailwheel and retractable landing gear which folded inwards.[1] Dalotel was assisted by Société Poulet in the construction of the prototype, registered F-PPZE, which was first flown in April 1969.[1] The aircraft was successfully tested during 1970 but despite efforts to market the aircraft none were ordered.[1] The aircraft was based at Meaux-Esbly airfield, to the west of Paris, for several years and was then sold to a pilot owner in the United Kingdom. Variants
Prototype with retractable landing gear and powered by a 165 hp (121 kW) Continental IO-346A piston engine, one built.[1]
Proposed variant with fixed landing gear and powered by a 125 hp (92 kW) engine, not built.[1]
Proposed variant with fixed landing gear and powered by a 160 hp (118 kW) engine, not built.[1]
Proposed variant of the DM-160 with retractable landing gear and constant speed propeller, not built.[1] Specifications (DM-165){{aerospecs|ref=[1] |met or eng?=met |crew=two |capacity= |length m=6.96 |length ft=22 |length in=10 |span m=8.40 |span ft=27 |span in=6¾ |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=1.76 |height ft=5 |height in=9¼ |wing area sqm=12.30 |wing area sqft=132.40 |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=1 |eng1 type=Continental IO-346A flat-four piston engine |eng1 kw=121 |eng1 hp=165 |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=300 |max speed mph=186 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }}{{aircontent |see also= |related= |similar aircraft= |sequence= |lists= }} ReferencesNotes1. ^1 2 3 4 5 6 7 8 9 {{Harvnb |Orbis|1985|p= 1300}} Bibliography{{refbegin}}
1 : French aircraft 1960–1969 |
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