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MORE ROCKETS.
MORE BUSINESS.
OUR LAUNCH SERVICES
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 early 2025.
BLOCK 1 (2025)
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Payload Mass: up to 215 kg (305 kg)
Orbits: 500 km SSO (500 km Equatorial Orbits)
No. of stages: 3
Payload Fairing: 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 110 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."
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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:
LAUNCH SITE
Bowen Orbital Spaceport, Australia
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Located at the Abbot Point State Development Area in Queensland, Australia.
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20- to 65-degree, low to mid inclination equatorial orbits.
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Preparing for a first orbital launch in 2024.