Williams V-Jet II

{{More footnotes|date=July 2008}}

{{Infobox aircraft

| name=Williams V-Jet II

| image= File:Scaled Composites 271 V-Jet II (N222FJ).jpg

| caption=

| type=Light jet

| national_origin=United States

| manufacturer=Williams International, Scaled Composites

| designer=Burt Rutan

| first_flight=1997

| introduction=1997

| retired=2001

| status=On display

| number_built=1

| unit cost=

| developed_into= Eclipse 500

| variants=

}}

The Williams V-Jet II was designed and built by Burt Rutan's Scaled Composites for Williams International as a test bed and demonstrator aircraft for Williams' new FJX-1 turbofan engine.{{cite web|title=Scaled Composites V-Jet II|url=http://www.scaled.com/projects/v-jet_ii|access-date=16 March 2011|archive-url=https://web.archive.org/web/20150520103753/http://www.scaled.com/projects/v-jet_ii|archive-date=20 May 2015|url-status=dead}}

Development

Williams International had been building small turbofan engines for cruise missile applications since the 1950s, and had successfully entered the general aviation market in the late 1980s with the FJ44 engine. In 1992, NASA initiated a program, Advanced General Aviation Transport Experiments (AGATE) to partner with manufacturers and help develop technologies that would revitalize the sagging general aviation industry. In 1996, Williams joined AGATE's General Aviation Propulsion (GAP) program to develop a fuel-efficient turbofan engine that would be even smaller than the FJ44. The result was the FJX-2 engine, which produced {{convert|550|lbf|abbr=on}} thrust.

Williams then contracted with Burt Rutan's Scaled Composites to design and build the V-Jet II, considered a Very Light Jet (VLJ), to use as a testbed and technology demonstrator to showcase the new engine.{{cite journal|journal=Popular Science|title=New Wings for the Jet Set|date=December 1997}} At Scaled, the aircraft was known as the Model 271. The aircraft and engine were debuted at the 1997 Oshkosh Airshow. Scaled's test pilot Doug Shane received the Iven C. Kincheloe Award from the Society of Experimental Test Pilots for his flight test work on the plane.

The V-Jet II was an all-composite structure with a forward-swept wing, a V-tail, each fin of which was mounted on the nacelle of one of the two engines. The overall design was quite reminiscent of the LearAvia Lear Fan, although much smaller.

Williams had not intended to produce the aircraft, but it attracted a lot of attention, and Eclipse Aviation was founded in 1998 to further develop and produce the aircraft. The airframe was significantly redesigned as an all-metal structure sporting a T-tail, and the name Eclipse 500. The prototype flew with a pair of EJ-22 engines, a variant of the FJX-2. However, performance was not satisfactory, and the design was changed to use two Pratt & Whitney Canada PW610F engines, which had been specifically designed by Pratt for the Eclipse.

The prototype and only V-Jet II aircraft was obtained by Eclipse Aviation along with the program, and was donated to the Experimental Aircraft Association AirVenture museum in Oshkosh, Wisconsin in 2001.

Specifications (V-Jet II)

{{Aircraft specs

|ref=

|prime units?=kts

|genhide=

|crew=

|capacity=

|length m=

|length ft=35

|length in=1

|length note=

|span m=

|span ft=35

|span in=4

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=118

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=2,200

|empty weight note=

|gross weight kg=

|gross weight lb=3,800

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Williams FJX-2

|eng1 type=turbofan

|eng1 kn=

|eng1 lbf=550

|eng1 note=

|power original=

|thrust original=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=300

|max speed note=

|max speed mach=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|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=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=

|ceiling ft=30,000

|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=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

}}

References

{{commons category}}

;Notes

{{Reflist}}

;Bibliography

  • [http://www.airventuremuseum.org/collection/aircraft/Williams%20V-Jet.asp EAA Museum page on prototype]
  • [http://www.eclipseaviation.com/ Eclipse Aviation website]

{{Scaled Composites}}

Category:Rutan aircraft

Category:Scaled Composites

Category:1990s United States experimental aircraft

Category:V-tail aircraft

Category:Eclipse aircraft

Category:Twinjets

Category:Forward-swept-wing aircraft

Category:Mid-wing aircraft

Category:Aircraft first flown in 1997