Pegasus Aeronautics Corporation

Supports: Profile · profileData.portfolioScope

Pegasus Aeronautics Corporation's documented portfolio in this dossier is bounded to Hybrid-electric propulsion for uncrewed aircraft and the source-backed functions listed below.

Supports: Profile · operating context

Pegasus provides a propulsion subsystem whose utility depends on aircraft integration, qualification, fuel, electrical and operational requirements.

Supports: Profile · commercial status

Pegasus presents GE-series products and continues federally supported development of propulsion for long-range fixed-wing VTOL aircraft.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

True North Map applies the VTOL tag from Pegasus Aeronautics Corporation's documented capability functions.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

Direct-drive propulsion This bounded statement is retained for reviewer verification.

Supports: Hybrid-electric propulsion for uncrewed aircraft · commercial availability

Pegasus Aeronautics Corporation currently presents Hybrid-electric propulsion for uncrewed aircraft through its official public capability surface.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

True North Map applies the hybrid-electric propulsion tag from Pegasus Aeronautics Corporation's documented capability functions.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

Fixed-wing and VTOL integration

Supports: Hybrid-electric propulsion for uncrewed aircraft · technicaldomainslugs

True North Map maps Hybrid-electric propulsion for uncrewed aircraft to aerospace and mobility from its documented technology functions.

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

Long-endurance uncrewed aircraft

Supports: Hybrid-electric propulsion for uncrewed aircraft · name

Hybrid-electric propulsion for uncrewed aircraft

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

Remote logistics This bounded statement is retained for reviewer verification.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

GE35 and GE70 product families

Supports: Hybrid-electric propulsion for uncrewed aircraft · summary

Pegasus develops hybrid gas-electric and direct-drive propulsion systems intended to extend endurance and payload utility for fixed-wing and multirotor uncrewed aircraft.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

Hybrid gas-electric power generation

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

Surveillance platforms This bounded statement is retained for reviewer verification.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

True North Map applies the direct drive tag from Pegasus Aeronautics Corporation's documented capability functions.

Supports: Hybrid-electric propulsion for uncrewed aircraft · capability type

Uncrewed-aircraft propulsion This bounded statement is retained for reviewer verification.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

True North Map applies the UAS endurance tag from Pegasus Aeronautics Corporation's documented capability functions.

Supports: Profile · operating context

Avartek's Boxer Hybrid integrates a Pegasus GE70 generator; the aircraft-specific description gives a 3.2 kW operating point at 25 kg, distinct from the standalone generator's maximum rating.

Supports: Profile · executive relevance summary

Source location: executiveRelevanceSummary

Avartek's Boxer Hybrid integrates a Pegasus GE70 generator; the aircraft-specific description gives a 3.2 kW operating point at 25 kg, distinct from the standalone generator's maximum rating.

Supports: Profile · executive relevance summary

Source location: executiveRelevanceSummary

The site lists a Waterloo operation at Unit 2, 560 Bathurst Drive and provides info@pegasusaero.ca and +1 604 812 7340.

Supports: Profile · operating context

The GE35 uses a 35 cc single-cylinder engine, weighs 2.6 kg and specifies 2 kW maximum versus 1–1.75 kW ideal output, with 22–50 V operation and liquid cooling.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technology readiness level

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · commercial availability

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technicaldomainslugs

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · name

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · core features

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · summary

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · capability type

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · maturity

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · technical tags

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · defence applications

GE35 is a 35 cc gas-electric range extender, 2.6 kg base weight, rated at 2,000 W maximum and 1,000–1,750 W ideal output, with 22–50 V operation. The liquid-cooled, fuel-injected, self-starting GE35 is offered for smaller multirotors and auxiliary fixed-wing power.

Supports: Hybrid-electric propulsion for uncrewed aircraft · maturity

NRCan contract CW2435733 awarded March 12, 2026 is C$106,333 for one G15 Sentinel UAV system for aerial filtered-water sampling; its stated term ends March 31, 2027.

Supports: Hybrid-electric propulsion for uncrewed aircraft · commercial availability

NRCan contract CW2435733 awarded March 12, 2026 is C$106,333 for one G15 Sentinel UAV system for aerial filtered-water sampling; its stated term ends March 31, 2027.