Javelin Overture: Difference between revisions
From MicrasWiki
Jump to navigationJump to search
No edit summary |
No edit summary |
||
| (One intermediate revision by the same user not shown) | |||
| Line 5: | Line 5: | ||
| titlestyle = margin:0;background-color:#7890BF;font-size:120%;font-weight:bold;border:1px solid #033E8C;text-align:center;color:#fff;padding:0.2em 0.4em; | | titlestyle = margin:0;background-color:#7890BF;font-size:120%;font-weight:bold;border:1px solid #033E8C;text-align:center;color:#fff;padding:0.2em 0.4em; | ||
| title = '''''{{PAGENAME}}''''' | | title = '''''{{PAGENAME}}''''' | ||
| image = | | image = [[File:Javelin-Overture-1720AN.png|250px]] | ||
| caption = [[Javelin Industries|Javelin]] | | caption = [[Javelin Industries|Javelin]] Overture in its maiden flight from [[Punta Santiago]] to [[Parap]] ({{AN|1693}}) | ||
| label2 = Type | | label2 = Type | ||
| data2 = | | data2 = Supersonic transport | ||
| label3 = Place of origin | | label3 = Place of origin | ||
| data3 = {{team flag|Nouvelle Alexandrie}} | | data3 = {{team flag|Nouvelle Alexandrie}} | ||
| label4 = | | label4 = Designers | ||
| data4 = {{Unbulleted list|[[Javelin Industries]]|[[Kerularios & Company]]}} | | data4 = {{Unbulleted list|[[Javelin Industries]]|[[Kerularios & Company]]}} | ||
| label5 = Manufacturer | | label5 = Manufacturer | ||
| Line 20: | Line 20: | ||
| data7 = {{AN|1689}} | | data7 = {{AN|1689}} | ||
| label8 = Introduction | | label8 = Introduction | ||
| data8 = | | data8 = {{AN|1692}} | ||
| label9 = Crew | |||
| data9 = 2 | |||
| label10 = Seating | |||
| data10 = 300 passengers | |||
| label11 = Length | |||
| data11 = 96.0 m | |||
| label12 = Wingspan | |||
| data12 = 43.9 m | |||
| label13 = Height | |||
| data13 = 18.6 m | |||
| label14 = Wing area | |||
| data14 = 880 m2 | |||
| label15 = Empty weight | |||
| data15 = 135,000 kg | |||
| label16 = Loaded weight | |||
| data16 = 226,800 kg | |||
| label17 = Fuel weight | |||
| data17 = 210,000 kg | |||
| label18 = Max takeoff weight | |||
| data18 = 350,000 kg | |||
| label19 = Powerplant | |||
| data19 = 4x J400 variable-cycle turbofans, 290 kN each | |||
| label20 = Cruise speed | |||
| data20 = Mach 3.2 | |||
| label21 = Range | |||
| data21 = 12,000 km | |||
| label22 = Service ceiling | |||
| data22 = 25,000 m | |||
| label23 = Rate of climb | |||
| data23 = 20 m/s | |||
| label24 = Wing loading | |||
| data24 = 397 kg/m2 | |||
| label25 = Thrust/weight | |||
| data25 = 0.33 | |||
| label25 = Take off distance | |||
| data25 = 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 {{AN|1692}}, with the [[Nouvelle Alexandrie|New Alexandrian]] airlines [[AirAlduria]] and [[AirImperial]] placing the first orders of the aircraft in {{AN|1693}}. | |||
==Orders== | |||
*{{AN|1692}} [[AirAlduria]], 12, ''delivered fully by XV.{{AN|1720}}''; | |||
*{{AN|1692}} [[AirImperial]], 10, ''started production on XV.{{AN|1720}}''. | |||
[[Category:Aircraft]] | [[Category:Aircraft]] | ||
[[Category:Javelin Industries]] | [[Category:Javelin Industries]] | ||
Latest revision as of 19:01, 30 May 2023
 Javelin Overture in its maiden flight from Punta Santiago to Parap (1693 AN) | |
| 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.
