MORE ROCKETS.

MORE BUSINESS.

Height:

25 m

Diameter: 1.2 or 1.5 m

Diameter: 1.5 m

Diameter: 2 m

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Gilmour Space's innovative Eris orbital launch vehicles will deliver up to 305 kg to LEO with a first commercial launch expected in 2022.

Payload Mass: up to 215 kg (305 kg)

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Orbits: 500 km SSO (500 km Equatorial Orbits) 

No. of stages: 3

Payload Fairing: 1.2 m or 1.5 m diameter with best in-class volume for relevant sized satellites.

Avionics: Precise controls using ERIS avionics and software algorithms/systems  developed from spaceflight-proven technologies.

Propulsion: Gilmour's new and proprietary hybrid rocket engine (test-fired to over 90 kN thrust).

"Our Gilmour Space Eris launchers are designed for production, ease of operation, and to provide customers with reliable and cost-effective access to space."

Adam Gilmour, CEO

Gilmour Space Technologies

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T+0s

First Stage Ignition

T+100s

Second Stage Ignition

T+200s

Second Stage Burnout

T+500s

Third Stage Ignition

T+620s

Orbital Insertion

TRAJECTORY: