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Javelin Sojourner: Difference between revisions

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===Civil===
===Civil===
*[[Javelin Industries]]:  
*[[Javelin Industries]]:  
**1x ''J-1050F(X)'' modified testbed for airborne trials of the [[Basilisk Glare]] directed-energy countermeasure suite (flown {{AN|1699}}–{{AN|1703}}, retired)
**1x ''J-1050F(X)'' modified testbed for airborne trials of the [[Basilisk Beam]] directed-energy countermeasure suite (flown {{AN|1699}}–{{AN|1703}}, retired)


===Military===
===Military===

Revision as of 19:54, 7 January 2022

Javelin Sojourner
Sojourner.jpg
Javelin J-1050 Sojourner.
Type Wide-body airliner
Place of origin Nouvelle Alexandrie Nouvelle Alexandrie
Designed
Manufacturer Javelin Industries
Crew 2 pilots
Seating 349 passengers (3-class)
Length 76.5 m
Height 19.7 m
Wingspan 71.8 m
Wing area 517 m2
Empty weight 145,000 kg
Fuel weight 159,000 kg
Max takeoff weight 344,000 kg
Powerplant 2x turbofans, 490 kN each
Max speed Mach 0.87
Cruise speed Mach 0.84
Range 17,560 km
Service ceiling 13,100 m
Wing loading 665 kg/m2

The Javelin J-1050 Sojourner is a widebody airliner designed by Javelin Industries. It is large, subsonic, and designed to have a long service range to cover long international flights around Micras.

The J-1050 is available in two versions. One version is the base passenger version that can handle 407 passengers in a 3-class layout. The other version is a freighter version, the J-1050F which can transport up to 102 metric tons of cargo. Beginning in 1704 AN the J-1050F has begun to commence delivery to air forces of the Benacian Union and Hurmu as part of orders placed under the Osman-Spiik Accord of 1703 AN. In military service the cargo transport variant has received the Raspur Pact designation of C-12 Sojourner.

Operators

Civil

Military