Gilmour Space's innovative and cost-effective ERIS launch vehicles will deliver up to 450 kg to LEO, with ERIS-S (up to 200 kg to 500 km SSO) followed by ERIS-L (450 kg to 180-500 km SSO).
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Contact us for a Payload User Guide in Q4 2019.
Height:
27 m
ERIS-S
Diameter: 1.2 m
Propulsion: Gilmour's new and proprietary hybrid rocket engine (test-fired to 80kN 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."
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Adam Gilmour, CEO
Gilmour Space Technologies
Payload Fairing: 1.2 m diameter with best in-class volume for relevant sized satellites.
Payload Mass: up to 200 kg
Orbits: 500 km SSO
No. of stages: 3
Avionics: Precise controls using ERIS avionics and software algorithms/systems developed from spaceflight-proven technologies.
Diameter: 1.8 m
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: