- Design and development
- Variants
- Specifications (YC-100 prototype)
- References
name=YC-100 Hirondelle | image= | caption= }}{{Infobox Aircraft Type | type=Single seat microlight | national origin=France | manufacturer= from plans | designer=Yves Chasle | first flight=1 May 1985 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Chasle YC-100 Hirondelle ({{lang|en|Swallow}}) is a French single seat microlight designed in the 1980s. Design and developmentYves Chasle worked as an Aérospatiale stress engineer and independently designed several light aircraft, starting with the Chasle YC-12 Tourbillon. His YC-100 Hirondelle is a largely wooden framed and fabric covered single-seat sports aircraft of conventional pusher layout. It has a strut braced high wing of constant chord with styrofoam ribs. The fuselage of the Hirondelle is a slender, rectangular cross-sectioned beam with the pilot's seat upon it ahead of the wing leading edge. Behind the pilot a central structure supports the wing just above head level; on its trailing edge, one of several types of small piston engine, with power outputs typically around {{convert|20|kW|hp|abbr=on|0}}, drives a pusher propeller. The fin is broad and straight-tapered and the horizontal tail is attached to the fuselage underside. The Hirondelle has a short, fixed tricycle undercarriage. Its first flight was on 1 May 1985, powered by a {{convert|18|kW|hp|abbr=on|0}} König SC 430 engine, a 430 cc (26.2 cu in), air-cooled, three-cylinder radial. The second prototype, built in Brazil, had a {{convert|22|hp|kW|abbr=on|order=flip|0}} JPX PUL 425/503 engine, a 212 cc (12.9 cu in) air-cooled flat-twin two stroke.[[3]] The number built is uncertain; in 2009 two examples, both YC-100s, appeared on European civil registers, one in Spain and one in France.[4] VariantsPlans for these were available but only the YC-100 is known to have been built. - YC-100
- As described below but could also be fitted with a {{convert|22|hp|kW|abbr=on|order=flip|0}} JPX PUL 425/503.
- YC-101
- As YC-100 but span increased to {{convert|9.35|m|ftin|abbr=on|0}}. Recommended engines were the JPX PUL 865, the {{convert|28|hp|kW|abbr=on|order=flip|0}} König SD 570 or the {{convert|30|hp|kW|abbr=on|order=flip|0}} KFM 107ER.
- YC-110
- Shorter span ({{convert|8.25|m|ftin|abbr=on|0}} wings with NACA 23015 section and Junkers type, two part, full span auxiliary airfoil ailerons or flaperons. Recommended engines as YC-100 and also the König SD 570.
- YC-111
- Longer span ({{convert|9.35|m|ftin|abbr=on|0}}) YC-110. Recommended engines were the König SD 570, KFM 107ER, JPX PUL 865 and also the Rotax 377 or 447, respectively {{convert|26|kW|hp|abbr=on|0}} and {{convert|29.4|kW|hp|abbr=on|1}}.
Specifications (YC-100 prototype){{Aircraft specs |ref=Jane's All the World's Aircraft 1988/89 |prime units?=met |crew=one |length m=5.43 |length note= |span m=8.30 |span note= |height m=1.71 |height note= |wing area sqm=11.25 |wing area note= |aspect ratio= |airfoil=3.20.16Y (an Aérospatiale V.16F variant) |empty weight kg=110 |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=210 |max takeoff weight note= |fuel capacity=24 l (6.3 US gal; 5.3 Imp gal) |more general=
|eng1 number=1 |eng1 name=König SC 430 |eng1 type=air-cooled three cylinder 430 cc (26.24 cu in) radial engine[3] |eng1 kw=18 |eng1 note= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=
|perfhide= |max speed kmh=130 |max speed note= |cruise speed kmh=100 |cruise speed note= |stall speed kmh=45 |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |power/mass= |more performance=
- Take-off run, grass: less than {{convert|100|m|ft|abbr=on|-1}}
- Landing run, grass: about {{convert|27|m|ft|abbr=on|-1}}
}}{{aircontent |see also= |related= |similar aircraft= |lists= }}References1. ^1 2 {{cite book |title= Jane's All the World's Aircraft 1988-1989|last= Taylor|pages=684, 689}} 2. ^1 {{cite book |title=European registers handbook 2010 |last= Partington |first=Dave |edition= |year=2010|publisher= Air Britain (Historians) Ltd|location= |isbn=978-0-85130-425-0|pages=691, 1171}}
[1][2] }}{{Chasle aircraft}} 6 : Ultralight aircraft|French sport aircraft 1980–1989|Chasle aircraft|High-wing aircraft|Single-engined pusher aircraft|Aircraft first flown in 1985 |