The only small launch vehicle to employ stage-combustion rocket engines resulting in unprecedented performance. Coupling simple architecture with cutting edge production technology results in a low cost to orbit for a dedicated small satellite launch vehicle.
1 x Launcher E-2, Liquid Oxygen (LOX) / Kerosene (RP-1)
1 x Launcher E-1 (Pressure fed), Liquid Oxygen (LOX) / Kerosene (RP-1)
150 kg (330 lbs) to 200 km, 28.5° orbit
105 kg (231 lbs) to 500 km SSO
The Launcher Light payload fairing is capable of accommodating an standard ESPA sized payload with ample margin with more room for any combination of additional small and Cube satellites.Download CAD Model
Launcher Light doesn’t cut corners to get to orbit. From the start, we are designing our E-2 engine as a closed-cycle, staged-combustion engine that powers the first stage with a single engine. This high efficiency engine enables a small, low cost rocket to carry a comparatively large amount of payload.
The entire assembled Launcher Light is ground transportable and can operate from globally dispersed launch sites with minimal to no permanent infrastructure.