Javelin F-18 Cyclone: Difference between revisions
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In the second month of 1700 Officials were obliged to confirm the existence of an airworthy prototype following widespread reports, sourced from eyewitness accounts, film footage and photographs, of an all-black jet delta winged aircraft of unknown configuration conducting flights from | In the second month of 1700 Officials were obliged to confirm the existence of an airworthy prototype following widespread reports, sourced from eyewitness accounts, film footage and photographs, of an all-black jet delta winged aircraft of unknown configuration conducting flights from | ||
La Columna Air Force testing site. | La Columna Air Force testing site. This was not however the finished design, but rather a testbed for proofing aerodynamic principles and evaluating the titanium based stressed metal fuselage, wings, and composite coating materials. | ||
[[Category:Weaponry]] | [[Category:Weaponry]] | ||
[[Category:Aircraft]] | [[Category:Aircraft]] |
Revision as of 19:48, 3 September 2021
![]() Design image of the F-18 Cyclone | |
Type | Strategic deep-strike fighter |
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Place of origin |
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Designed | 1697 AN – 1700 AN |
Manufacturer | Cyclone Compact consortium |
The Javelin F-18 Cyclone is a proposed fighter aircraft concept that is under development in Nouvelle Alexandrie and Ransenar for the Federal Forces of Nouvelle Alexandrie and the Royal Ransenari Armed Forces. It is being developed under by a consortium known as the "Cyclone Compact", consisting of the New Alexandrian Department of Defense, the National Science Administration, Javelin Industries, the Ransenari Ministry of Defense, MetaAvionics, and Kerularios & Company.
Development & production timeline
In the second month of 1700 Officials were obliged to confirm the existence of an airworthy prototype following widespread reports, sourced from eyewitness accounts, film footage and photographs, of an all-black jet delta winged aircraft of unknown configuration conducting flights from La Columna Air Force testing site. This was not however the finished design, but rather a testbed for proofing aerodynamic principles and evaluating the titanium based stressed metal fuselage, wings, and composite coating materials.