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词条 ATG Javelin
释义

  1. Specifications (Javelin MK-10)

  2. See also

  3. References

  4. External links

name= Javelinimage=CPJavelin.jpgcaption= Javelin mockup on display at Reno Air Show

}}{{Infobox Aircraft Type

type= Civil utility aircraft and Militarymanufacturer= Aviation Technology Groupdesigner=first flight= September 30, 2005introduced=retired=status= Canceledprimary user=more users=produced=number built=unit cost= US$2,995,000variants with their own articles=
}}

The ATG Javelin was an American small high-speed personal jet that was developed by the Aviation Technology Group (ATG) prior to its bankruptcy. Planned for FAA certification under 14 CFR part 23, the Javelin had a design resembling a fighter aircraft, an unusual concept for civilian jets. The Javelin MK-20 derivative, developed in cooperation between ATG and Israel Aerospace Industries, was expected to fill the jet trainer role for various air forces. The first prototype took flight on 30 September 2005.

ATG halted all further development on the Javelin in December 2007 after failing to get $200 million to finance further development.[1] The company subsequently declared bankruptcy in 2008, ending the development of the Javelin.

Javelin design rights were bought by Rud Aero, a very small airplane manufacturer. They have partnered with another very small firm, Stavatti Aerospace to offer a variant of the Javelin for the U.S. Air Force's T-X program.

Specifications (Javelin MK-10)

{{Aircraft specifications
|plane or copter?=plane
|jet or prop?=jet
|crew=2
|capacity=2
|length main=37 ft 0 in
|length alt=11.28 m
|span main=25 ft 1 in
|span alt=7.65 m
|height main=10 ft 6 in
|height alt=3.20 m
|area main=140 ft²
|area alt=13 m²
|empty weight main= 4,655 lb
|empty weight alt= 2 111 kg
|loaded weight main=
|loaded weight alt=
|max takeoff weight main=6,900 lb
|max takeoff weight alt= 3 100 kg
|number of jets=2
|engine (jet)=Williams FJ33-4-19J
|type of jet=turbofans
|thrust main=1,750 lbf
|thrust alt=8.0 kN
|max speed main=500 knots
|max speed alt=575 mph, 925 km/h
|range main=1,000 nm
|range alt=1,151 mi, 1,852 km
|ceiling main=45,000 ft
|ceiling alt=13 700 m
|climb rate main=9,000 ft/min
|climb rate alt=46 m/s
|max loading main=46 lb/ft²
|max loading alt=220 kg/m²
|max thrust/weight=0.56
}}

See also

{{Aircontent
|similar aircraft=
  • Bede BD-10
  • Viper Aircraft ViperJet

|lists=
|see also=
  • Very light jet

}}

References

1. ^Flight Global: Lack of funds halts ATG's Javelin VLJ

External links

{{Commons category|ATG Javelin}}
  • Israel Aircraft Industries
  • [https://web.archive.org/web/20051029090829/http://www.appliedcompositetechnology.com/ ACTA]
  • Airframer.com: ATG Javelin program suppliers
  • Airframer.com: ATG Press Release, March 4, 2008

9 : United States civil utility aircraft 2000–2009|Very light jets|Cancelled aircraft projects|Twinjets|ATG aircraft|Low-wing aircraft|Aircraft first flown in 2005|Projects established in 2005|Projects disestablished in 2007

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