| Variant | MQ-25A |
| Role | carrier based refueling |
| Country | USA |
| Builder | Boeing |
| Industry Team |
Aitech Defense Systems
Astronics
BAE Systems
Collins Aerospace
Cox & Company
Crane Aerospace & Electronics
Cubic
Curtiss-Wright Defense Solutions
GE
Harris Corporation
Héroux-Devtek
Honeywell
Innovative Power Solutions
L3 Commercial Aviation
Moog Aircraft Group
Parker Hannifin
Raytheon
Rolls-Royce
Triumph Group
|
| First Flight | September 19, 2019 |
| Status | production |
| IOC | 2026 |
| Number built | 72 planned |
| Operators | US Navy |
| Cost | $15.2 billion |
| Comparable Aircraft | none |
| Recognition | |
| Wingspan | 12 meters | 39.4 feet |
| Sweep | |
| Wing Aspect Ratio | |
| Fuselage Maximum Diameter | meters | feet |
| length | 19 m meters | 62.34 feet |
| height | 3.5 meters | 11.5 feet |
| wing area | sqm | sqfeet |
| Weight empty | 6,400 kg | 14,000 lb |
| takeoff (clean) | kg | lb |
| takeoff (maximum) | 20,200 kg | 44,500lb |
| Fuel, Internal | kg | lb |
| Fuel, External | kg | lb |
| Payload | kg | lb |
| Max weapon load | kg | lb |
| Armament | |
| Power Plant | 1 x Rolls-Royce AE 3007N Turbofan Engine |
| Thrust, max, SLS, ISA | x kg | x lbst |
| Internal fuel (usable) | kg | lb |
| Performance (clean, ISA) | |
| Max level speed (sea level) | 335 KTAS / 620 km/hr |
| Limit speed | KEAS / MN |
| Stall speed (landing, 20% fuel) | 90 KCAS |
| Stall speed (reference) | KCAS |
| Rate of climb (SL) | feet/min |
| Service ceiling | 12,000 meters | 39,000 feet |
| Range / 3 ext. tanks (10% reserve) | km | nm |
| Range, ext. tanks | km | nm |
| Range, clean | 4,000 km | 2,200 nm |
| Endurance, clean / ext. tanks | h min / hr |
| Max sustained Load Factor (S.L.) | g |
| Max sustained Load Factor (15,000 feet) | g |
| Max sustained Turn Rate (15,000 feet) | deg/sec |
| Takeoff ground run (S.L.) | meters | feet |
| Landing ground roll (S.L., 20% internal fuel) | meters | feet |
| Limit Load factor | + g / - g |
| Crew | 0 |
| Accomodations | 0 |
