02 / SMALL-LIFT VEHICLE
OLYMPUS
Compact launch capability, engineered for precision.
Olympus is the CERES small-lift launch vehicle. At 25 metres long and 2 metres in diameter, it uses liquid oxygen and liquid methane propellants in a compact, responsive launch system.
2 M
VEHICLE DIAMETER
25 M
VEHICLE LENGTH
LOX / LCH4
LIQUID OXYGEN + LIQUID METHANE
OLYMPUS / STAGE SEPARATION SEQUENCE
03 / VEHICLE SYSTEMS
ENGINES
Designed around the compact geometry of a small-lift vehicle, the Olympus engine system integrates propulsion, guidance, and vehicle control into a tightly packaged launch architecture.
COMPACT
ENGINE ARCHITECTURE
CONTROLLED
ASCENT PERFORMANCE
PROPULSION
Olympus is powered by liquid oxygen and liquid methane. This propellant combination supports high-performance combustion and a cleaner operational pathway for a responsive launch system.
LOX / LCH4
LIQUID OXYGEN + LIQUID METHANE
04 / LAUNCH CONFIGURATIONS
CHOOSE YOUR LAUNCH PROFILE
Fly with the Olympus profile that best matches your payload, schedule, and target orbit.
01
DEDICATED
Reserve the full Olympus launch for one payload, with mission timing and target orbit shaped around your spacecraft.
02
RIDESHARE
Share an Olympus launch with compatible payloads on an efficient, coordinated path to orbit.
01 / TRAJECTORY
The future of launch runs on precision, cadence, and certainty.
48 HRS
TARGET TURNAROUND
1000 KG
TO LOW EARTH ORBIT
2028
FIRST COMMERCIAL FLIGHT
MISSION PLANNING
Plan a mission with OLYMPUS.
CONTACT MISSION TEAM