Solution dossier / Hybrid UAV power units

Pegasus GE35 and GE70 Hybrid UAV Power Units

Gas-electric power units for UAVs, with published maximum continuous electrical outputs of 2,000 W and 4,000 W, subject to platform integration.

Owned or delivered by Pegasus Aeronautics Corporation

· Updated

Evidence status
Company sources reviewed
Last reviewed
October 8, 2026
Public sources
6
Source coverage
Solution-specific
Domains
Air
Scope boundary: Manufacturer specifications depend on configuration and aircraft integration. Product pages and brochures publish different voltage figures; confirm the applicable installation requirements.

The GE35 and GE70 are gas-electric power units from Canadian manufacturer Pegasus Aeronautics. They generate electrical power for unmanned aerial vehicles, combining a gasoline engine with electrical power management. Pegasus describes the hybrid architecture as supplying onboard loads while managing battery state of charge. Hybrid power architecture.

GE35 and GE70 specifications

The GE35 serves the smaller power requirement, while the GE70 provides a higher electrical output using a larger engine. Pegasus publishes the following figures in its product pages and brochures:

Published specification GE35 GE70
Engine Single-cylinder, two-stroke Two-cylinder, two-stroke
Displacement 35 cc 70 cc
Base dry weight 2.60 kg 3.50 kg
Maximum continuous electrical output, brochure figure 2,000 W 4,000 W
Ideal power range, product-page figure 1,000–1,750 W 2,000–3,500 W
Initial time between overhauls 200 hours 200 hours

Sources: GE35 product page, GE70 product page, GE35 brochure and GE70 brochure. The brochures state that electrical output varies with platform integration. Base dry weight is not the weight of a complete fuelled aircraft installation.

The published voltage figures need clarification for a specific installation. The GE35 webpage lists 22–50 V and the GE70 webpage lists 50 V, while both brochures specify 24–50 V. These are different published specifications; the applicable voltage and configuration should be confirmed with Pegasus during integration.

Interfaces, cooling and maintenance

Both brochures describe fuel injection, liquid cooling and automatic throttle adjustment in response to electrical demand. They list CAN, serial and PWM control interfaces, including remote starting and options for redundant control connections. These functions connect the generator with the aircraft’s power and control systems. The 200-hour maintenance figure is presented as an initial time between overhauls. GE35 technical brochure, GE70 technical brochure.

How the GD70 differs

Pegasus’s GD70 is a direct-drive propulsion unit with auxiliary electrical generation. Its product page lists 4,500 W of mechanical output and 500 W of electrical output, with a 1,000 W electrical peak. The 4,500 W figure therefore refers to shaft power; it is not comparable to the GE35 and GE70 electrical-output ratings. GD70 specifications.

Evidence

Pegasus GE35 and GE70 Hybrid UAV Power Units source register

Each source below supports a bounded part of this record. A link is not an endorsement by its publisher.

  1. 01

    Hybrid power architecture

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    Hybrid generation, onboard electrical-load supply and battery state-of-charge management.

  2. 02

    GE35 product page

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    GE35 engine, ideal power range and webpage voltage specification of 22–50 V.

  3. 03

    GE70 product page

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    GE70 engine, ideal power range and webpage voltage specification of 50 V.

  4. 04

    GE35 brochure

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    GE35 base dry mass, maximum continuous electrical output, 24–50 V brochure figure, interfaces, cooling and initial TBO; output varies with integration.

  5. 05

    GE70 brochure

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    GE70 base dry mass, maximum continuous electrical output, 24–50 V brochure figure, interfaces, cooling and initial TBO; output varies with integration.

  6. 06

    GD70 specifications

    Pegasus Aeronautics · Company · Undated · Accessed October 8, 2026

    GD70 mechanical output of 4,500 W; electrical output of 500 W with 1,000 W peak.

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