Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Martin X-24B Lifting Body Technology Demonstrator Aircraft.
1 x XLR-11-RM-13 rocket engine developing 9,800lb of thrust; OPTIONAL: 2 x Bell LLRV landing rockets developing 500lb of thrust each.
Propulsion
1,165 mph
1,875 kph | 1,012 kts
Max Speed
74,147 ft
22,600 m | 14 miles
Service Ceiling
47 miles
75 km | 40 nm
Operational Range