Gilmour Space's innovative Eris orbital launch vehicles will deliver up to 305 kg to LEO.
Stats
Height: 25 m
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
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).
Courtesy of Gilmour Space.