https://discord.com/channels/909034158205059082/1347411688047247502
https://discord.com/channels/909034158205059082/1348093032909770804
The Ifrit is described as highly capable as an air superiority fighter, and to understand how it should be balanced we need to keep it’s heritage- a stealth, twin engine, high performance 5th generation fighter- firmly in context.
The Ifrit struggles to achieve the high speeds at altitude that twin engine 5th gen fighters are known for. At 40k ft, the F-22A can achieve Mach 2.2 with a combat load. The Su-57 and J-20A supposedly hit Mach 2, according to official stats. The Ifrit over speeds at Mach 1.72 (which is Mach 1.9 IRL) at the same altitude, far below what the maximum emergency speed should be for a fighter of its type.
It took me the full length of the map to reach Mach 1.32 (1.5 IRL) at 99% throttle in the Ifrit at 40k ft, again, significantly below the capabilities of the aircraft the Ifrit is based on. Meanwhile, according to AirForceNews (1999), "Sustaining the target Mach was not difficult for the Raptor," said Col. C.D. Moore, Combined Test Force commander, at Edwards Air Force Base, Calif. "The difficulty was keeping the Raptor from going faster than the target speed. Yesterday the airplane demonstrated that it can achieve awesome speed, flying above 1.5 Mach at a low power setting, for a sustained period of time.”
The Ifrit struggled to reach the above speeds. It felt sluggish to accelerate at this altitude, incredibly easy to bleed speed, and would often drop subsonic seconds into a 6G turn. I understand that the Ifrit has had its speed/drag tinkered with to make sure it’s not too powerful, but this is absolutely ridiculous. A clean Ifrit should be highly capable at altitudes above 20,000 feet, and should have greater energy retention, acceleration, and max speed at high altitudes.
Edit: [Start here](#1348138478805712977 message)


