<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> {{Infobox aircraft | name = Eclipse | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = [[Ultralight trike]] | aim = | outcome = | related = | national_origin = [[United States]] | manufacturer = [[Buckeye Industries]] | design_group = | designer = | builder = | issuer = | status = Production completed | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} The '''Buckeye Eclipse''' and '''Buckeye Endeavor''' are a family of [[United States|American]] two-seat [[flying wing]] [[ultralight trike]]s that was designed and produced by [[Buckeye Industries]]. The aircraft were supplied fully assembled.<ref name="Cliche">Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page C-6. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}</ref>
==Design and development== Buckeye Industries was well known in the US ultralight business as one of the leading manufacturers of [[powered parachute]]s in the 1980s and 90s. The company decided to expand their line with the introduction of a line of trikes in the late 1990s. The aircraft were not strong sellers and the company went out of business in the mid-2000s.<ref name="Cliche" />
The Eclipse features a [[Flying wires|cable-braced]] [[hang glider]]-style [[high-wing]], weight-shift controls, a single-seat, open cockpit, [[tricycle landing gear]] and a single engine in [[pusher configuration]]. Factory-supplied standard equipment included dual controls and electronic flight instruments. Optional equipment included a [[fiberglass]] cockpit [[Aircraft fairing|fairing]], windshield, [[wheel pants]] and electric starter.<ref name="Cliche" />
The aircraft carriage is made from welded [[4130 steel]] tubing, while the wing is constructed from bolted-together [[aluminum]] tubing and covered in [[Dacron]] sailcloth. The {{convert|167|sqft|m2|abbr=on}} area wing is supported by a single tube-type [[kingpost]] and uses an "A" frame control bar.<ref name="Cliche" /> <!-- ==Operational history== -->
==Variants== ;Eclipse :Basic model powered by a [[Rotax 503]] twin cylinder, air-cooled, [[two-stroke]] engine of {{convert|50|hp|kW|0|abbr=on}}, with a gross weight of {{convert|850|lb|kg|0|abbr=on}}. Price was [[US$]]14,500 in 2000.<ref name="Cliche" /> ;Endeavor :Up-market model powered by a [[Rotax 582]] twin cylinder, liquid-cooled, two-stroke engine of {{convert|64|hp|kW|0|abbr=on}}, with a gross weight of {{convert|1000|lb|kg|0|abbr=on}}. Price was US$16,300 in 2000.<ref name="Cliche" /> <!-- ==Aircraft on display== -->
==Specifications (Endeavor) == {{Aircraft specs |ref=Cliche<ref name="Cliche" /> |prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> <!-- General characteristics --> |genhide=
|crew=one |capacity=one passenger |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=167 |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=260 |empty weight note= |gross weight kg= |gross weight lb=1000 |gross weight note= |fuel capacity={{convert|10|u.s.gal}} |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=[[Rotax 582]] |eng1 type=twin cylinder, liquid-cooled, [[two-stroke]] [[aircraft engine]] |eng1 kw=<!-- prop engines --> |eng1 hp=64<!-- prop engines -->
|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop note=
<!-- Performance --> |perfhide=
|max speed kmh= |max speed mph= |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph=75 |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph=27 |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range km= |range miles= |range nmi= |range note= |endurance=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin=700 |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= |thrust/weight= |more performance= |avionics= }}
<!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}
==References== {{reflist}}
<!-- ==External links== --> {{Buckeye Industries aircraft}}
[[Category:1990s United States ultralight aircraft]] [[Category:Single-engined pusher aircraft]] [[Category:Ultralight trikes]]