Van's Aircraft RV-8

{{Short description|American kit aircraft}}

{{Use mdy dates|date=November 2022}}

{{Use American English|date=November 2022}}

{{Infobox aircraft

|name = RV-8

|logo =

|image = VansRV-8C-GERV02.jpg

|caption =

|type = RV-8

|manufacturer = Van's Aircraft

|national_origin=United States

|designer = Richard VanGrunsven

|first_flight = 1995{{cite web|url= http://vansaircraft.com/public/rv8.htm |title= Total Performance RV Kit Planes |publisher= Van's Aircraft |access-date= 2012-08-21}}

|introduction = 1995

|retired =

|status =

|primary_user =

|more_users =

|produced =

|number_built = 1611 (November 2021){{cite web|url = https://www.vansaircraft.com/public/first-flights.htm|title = First Flights|access-date = 18 November 2021|last = Vans Aircraft |date = November 2022 }}

|developed_from = Van's Aircraft RV-4

|variants =

}}

File:Vans RV-8A N98VR Hondo TX 2007 Jun 02.jpg

File:RV8WS.JPG

File:RV-8.jpg

File:Vans RV8 Takeoff.jpg

The Van's RV-8 is a tandem two-seat, single-engine, low-wing homebuilt aircraft sold in kit form by Van's Aircraft. The RV-8 is equipped with conventional landing gear, while the RV-8A version features tricycle landing gear. The design is similar to the earlier RV-4, although it is larger than that earlier model.{{Citation | last = Downey | first = Julia | title = 2008 Kit Aircraft Directory | section = Kitplanes | volume = 24 | number = 12 | date = December 2007 | page = 77 | publisher = Primedia | ISSN = 0891-1851}}.Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Vol. 28, No. 12, December 2011, p. 74. Belvoir Publications. {{ISSN|0891-1851}}Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, p. 125. WDLA UK, Lancaster UK, 2011. {{ISSN |1368-485X}}

Development

Richard VanGrunsven designed the RV-8 series as an updated, larger tandem aircraft based on the RV-4 design concept. The RV-8 first flew in 1995 and was first shown publicly at Oshkosh that year.

The RV-8 incorporated changes as a result of lessons learned in producing the popular RV-4 design. The RV-8 airframe accepts larger engines from {{convert|150|to|210|hp|kW|0|abbr=on}}, including the {{convert|210|hp|kW|0|abbr=on}} Lycoming IO-390.{{cite web|url=https://www.vansaircraft.com/rv-8/ |title=Van's RV-8 |publisher=Van's Aircraft|access-date= 27 September 2020}} The RV-8 also has increased wingspan and wing area over the RV-4, as well as greater cockpit width, headroom, legroom and an increased useful load, all with a view to accommodating larger pilots. Like the RV-3 to RV-7 that preceded it, the RV-8 is stressed for aerobatics.

The RV-8 series was intended from inception to include a nose-gear-equipped version designated the RV-8A. The RV-8A was first flown in 1998

As of November 2022, 1,611 RV-8s and RV-8As have been completed and flown.

Specifications (RV-8)

{{Aircraft specs

|ref=Van's Aircraft{{cite web|url=http://vansaircraft.com/public/rv8specs.htm |title=Van's Aircraft - RV-8 Specifications |publisher=Vansaircraft.com |access-date=2012-08-21}}{{cite web|url=http://vansaircraft.com/public/rv8perf.htm |title=Van's Aircraft - RV-8 Performance |publisher=Vansaircraft.com |access-date=2012-08-21}}

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=21

|length in=0

|length note=

|span m=

|span ft=24

|span in=0

|span note=

|height m=

|height ft=5

|height in=7

|height note=

|wing area sqm=

|wing area sqft=116

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=1120

|empty weight note=

|gross weight kg=

|gross weight lb=1800

|gross weight note=

|fuel capacity={{convert|42|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Lycoming IO-360

|eng1 type=four cylinder, horizontally opposed piston aircraft engine with fuel injection

|eng1 kw=

|eng1 hp=200

|eng1 shp=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

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|perfhide=

|max speed kmh=

|max speed mph=221

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=210

|cruise speed kts=

|cruise speed note=at 75% power at 8000 feet

|stall speed kmh=

|stall speed mph=58

|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=940

|range nmi=

|range note=at 55% power and 8000 feet

|endurance=

|ceiling m=

|ceiling ft=22500

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1900

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=15.5

|wing loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

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|more performance=

|avionics=

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See also

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References

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