Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Hermeus Quarterhorse Hypersonic Test Vehicle.
1 x Pratt & Whitney F100 (JTF22) afterburning turbofan engine developing approximately 18,000lb of thrust dry and 30,000lb of thrust with reheat; 1 x Ramjet engine of unknown make, model, and output power.
Propulsion
5,748 mph
9,250 kph | 4,995 kts
Max Speed
3,728 mph
6,000 kph | 3,240 kts
Cruise Speed