Design Requirements
Your submission must depict an aircraft which entered operational service between January 1995 and December 2015.

The aircraft should be a 4.5 Generation aircraft, that is an aircraft that incorporates some features of fifth generation designs but lacks others such as all-aspect stealth. Such capabilities may include advanced sensor integration, AESA radar, supercruise capability, supermaneuverability, broad multi-role capability, and reduced radar cross-section.


The maximum takeoff weight of the aircraft must not exceed 40,000 lbs (18000 kg)

The aircraft should be primarily designed to fulfill air-to-air fighter missions, but can also be able to conduct other missions.