| 词条 | Robin HR100 | |||||||||||||||||
| 释义 |
The Robin HR100 is a French four-seat light monoplane built by Avions Pierre Robin as metal-winged version of the Robin DR253 Regent. DevelopmentThe prototype of the Robin HR100 was the prototype DR253 Regent which was rebuilt with metal wings and powered by a 180 hp (134 kW) Lycoming O-360 engine. It first flew on 3 April 1969 as the Robin HR100/180. The HR100 is a low-wing cantilever monoplane with a conventional cantilever tail unit and a fixed tricycle landing gear. A number of different variants were produced in the 1970s. From 1972 a high-powered improved version was produced as the HR100/285 with a 285 hp (213 kW) Continental Tiara 6-285B engine and retractable landing gear and airframe modifications. The French Air Force ordered a number of HR.100/250 aircraft in the mid 1970s and these were used for communications and other duties. A two-seat trainer version was developed as the HR200, and a modified version with a lighter airframe and new fin and rudder was developed as the R1180 Aiglon in 1977. Variants
1969 Prototype with a 180hp (134kW) Lycoming O-360 engine, one built.
1976 Prototype with a 180hp (134kW) Lycoming O-360 engine, one built.
Initial production version with a 200hp (149kW) Lycoming IO-360 engine.
Production version with a 210hp (157kW) engine, 113 built of both 200B Royal and 210 Safari variants.
Experimental HR.100 with an enlarged tail and retractable landing gear and a 235hp Lycoming O-540-B engine, one built.
HR.100/235 with a 250hp (186kW) Lycoming IO-540-C4B5 engine, 24 built.
HR.200/235 with a 285hp (213kW) Continental Tiara 6-285 engine, 37 built
Experimental version with two extra children's seats, one built OperatorsMilitary operators
Specifications (HR.100/285){{aerospecs|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2799 |met or eng?=met |crew= |capacity=4 |length m=7.59 |length ft=24 |length in=10¾ |span m=9.08 |span ft=29 |span in=9½ |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=2.71 |height ft=8 |height in=10¾ |wing area sqm=15.20 |wing area sqft=163.62 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=840 |empty weight lb=1852 |gross weight kg=1400 |gross weight lb=3086 |lift kg= |lift lb= |eng1 number=1 |eng1 type= Teledyne Continental Tiara 6-285 flat-six piston engine |eng1 kw=213 |eng1 hp=285 |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=325 |max speed mph=202 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=2130 |range miles=1323 |endurance h= |endurance min= |ceiling m=5700 |ceiling ft=18,700 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|see also= |related=
|similar aircraft= |sequence= |lists= }} References{{commons category|Robin HR100}}
5 : French civil utility aircraft 1960–1969|Robin aircraft|Aircraft first flown in 1969|Single-engined tractor aircraft|Low-wing aircraft |
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