Height:
30 m
Diameter: 1.2 or 1.5 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.
ERIS
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.
Diameter: 1.5 m
Propulsion: Gilmour's new and proprietary hybrid rocket engine (test-fired to 80kN thrust).
Diameter: 2 m
"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
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: