Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Hermeus Darkhorse Unmanned / Uncrewed Hypersonic Test Vehicle.
2 x Chimera II (Pratt & Whitney F100 turbofan core) ramjet engine of unknown thrust output.
Propulsion
3,837 mph
6,175 kph | 3,334 kts
Max Speed
2,495 mph
4,015 kph | 2,168 kts
Cruise Speed
111,549 ft
34,000 m | 21 miles
Service Ceiling
3,728 miles
6,000 km | 3,240 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).