Diameter: 1.2 or 1.5 m
Diameter: 1.5 m
Diameter: 2 m
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)
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
First Stage Ignition
Second Stage Ignition
Second Stage Burnout
Third Stage Ignition