Javelin Overture
| Javelin Overture | |
| Type | Supersonic transport |
|---|---|
| Place of origin |
 Nouvelle Alexandrie |
| Designers | |
| Manufacturer | Javelin Industries |
| Designed | 1681 AN-1688 AN |
| Testing | 1689 AN |
| Introduction | 1692 AN |
| Crew | 2 |
| Seating | 300 passengers |
| Length | 96.0 m |
| Wingspan | 43.9 m |
| Height | 18.6 m |
| Wing area | 880 m2 |
| Empty weight | 135,000 kg |
| Loaded weight | 226,800 kg |
| Fuel weight | 210,000 kg |
| Max takeoff weight | 350,000 kg |
| Powerplant | 4x J400 variable-cycle turbofans, 290 kN each |
| Cruise speed | Mach 3.2 |
| Range | 12,000 km |
| Service ceiling | 25,000 m |
| Rate of climb | 20 m/s |
| Wing loading | 397 kg/m2 |
| Take off distance | 3,300m |
The Javelin Overture, designated as J-6000, marks the debut of Javelin Industries into the realm of supersonic transport, designed by a joint venture between Javelin Industries and Kerularios & Company. Masterfully engineered to hit the speeds of Mach 3.2 while soaring at altitudes exceeding 20,000 meters, the J-6000 boasts a range of 12,000 kilometers, with the capacity to comfortably accommodate up to 300 passengers, adhering to a mixed-class seating arrangement.
The J-6000 signifies a quantum leap in supersonic transportation technology. It has an excellent cruising velocity, augmented fuel economy, and drastically minimized sonic boom and takeoff noise signatures. These enhanced features imbue the J-6000 with the competitive edge required to rival the widebody subsonic airliners of the current era, particularly in the sphere of long-range intercontinental transit.
The aircraft was introduced in 1692 AN, with the New Alexandrian airlines AirAlduria and AirImperial placing the first orders of the aircraft in 1693 AN.
Orders
- 1692 AN AirAlduria, 12, delivered fully by XV.1720 AN;
- 1692 AN AirImperial, 10, started production on XV.1720 AN.
