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Description
ATG Javelin USAF

The ATG Javelin was a 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.

Specifications (Javelin MK-10)

General characteristics

* Crew: 2
* Capacity: 2
* Length: 37 ft 0 in (11.28 m)
* Wingspan: 25 ft 1 in (7.65 m)
* Height: 10 ft 6 in (3.20 m)
* Wing area: 140 ft² (13 m²)
* Empty weight: 4,655 lb (2 111 kg)
* Max takeoff weight: 6,900 lb (3 100 kg)
* Powerplant: 2× Williams FJ33-4-19J turbofans, 1,750 lbf (8.0 kN) each

Performance

* Maximum speed: 500 knots (575 mph, 925 km/h)
* Range: 1,000 nm (1,151 mi, 1,852 km)
* Service ceiling: 45,000 ft (15 000 m)
* Rate of climb: 9,000 ft/min (46 m/s)
* Max wing loading: 46 lb/ft² (220 kg/m²)
* Minimum thrust/weight: 0.56

Description
ATG Javelin USAF

The ATG Javelin was a 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.

Specifications (Javelin MK-10)

General characteristics

* Crew: 2
* Capacity: 2
* Length: 37 ft 0 in (11.28 m)
* Wingspan: 25 ft 1 in (7.65 m)
* Height: 10 ft 6 in (3.20 m)
* Wing area: 140 ft² (13 m²)
* Empty weight: 4,655 lb (2 111 kg)
* Max takeoff weight: 6,900 lb (3 100 kg)
* Powerplant: 2× Williams FJ33-4-19J turbofans, 1,750 lbf (8.0 kN) each

Performance

* Maximum speed: 500 knots (575 mph, 925 km/h)
* Range: 1,000 nm (1,151 mi, 1,852 km)
* Service ceiling: 45,000 ft (15 000 m)
* Rate of climb: 9,000 ft/min (46 m/s)
* Max wing loading: 46 lb/ft² (220 kg/m²)
* Minimum thrust/weight: 0.56