

| Name | XRQ-72 Hybrid Electric Aircraft |
| Manufacturer | Northrop Grumman |
| Country of Origin | United States |
| Type / Role | ISR / Technology Demonstrator UAS |
| First Flight / Introduced | Under DARPA testing phase |
| Status | Experimental |
| Unit Cost | Not Disclosed |
| Maximum Speed | ~200 km/h |
| Cruise Speed | ~160 km/h |
| Operational Range | Mission dependent |
| Endurance | 12+ hours |
| Service Ceiling | ~25,000 ft |
| Rate of Climb | Not Disclosed |
| Length | Not Disclosed |
| Wingspan | Not Disclosed |
| Height | Not Disclosed |
| Maximum Takeoff Weight (MTOW) | ~570 kg class |
| Payload Capacity | ISR payloads only |
| Hardpoints | None |
| Weapons | None |
| Sensors | EO/IR, ISR sensor suite |
| Avionics | GPS, autonomous flight control |
| Engine Type | Fuel generator plus electric motors |
| Engine Power | Not Disclosed |
| Propeller Type | Electric driven propulsor |
| Control Type | Remote and autonomous |
| Data Link Range | Line of sight and satellite |
| Navigation | GPS and INS |
| Ground Control Station | Fixed or mobile |
| Primary Users | U.S. research agencies |
| Combat Proven | No |
| Notable Operations | Flight testing and evaluation |
The XRQ-72 hybrid electric aircraft is a U.S. experimental uncrewed platform designed to test how hybrid propulsion can extend endurance while lowering acoustic and thermal signatures. Built as a flying wing for efficiency and low observability, the aircraft supports intelligence, surveillance, and reconnaissance missions where persistence and discretion matter.
Northrop Grumman, in partnership with DARPA under the Series Hybrid Electric Propulsion Aircraft Demonstration effort.
Estimated cruise near 200 km per hour based on Group 3 UAS class performance.
Designed for extended endurance missions exceeding 12 hours, with operational range dependent on mission profile and power settings.
Prototype research platform. Unit cost not publicly disclosed.
The XRQ-72 uses a series hybrid layout. A fuel engine generates electricity, which powers electric motors that turn the propulsors. This allows efficient fuel use, flexible power management, and quieter operation than conventional designs. The flying wing shape reduces drag and radar return while providing internal volume for batteries, generators, and sensors.
Intended roles include ISR, communications relay, and technology validation for future military aircraft. The platform helps evaluate how hybrid systems perform in real flight conditions, including thermal management, endurance pacing, and signature control. Lessons from XRQ-72 are expected to inform next generation uncrewed aircraft where endurance, survivability, and efficiency are priorities.
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