Specifications are for 1000kg to Sun-Synchronous Orbit, or 200kg to Low-Earth Orbit. First flight is planned for 2024. Booster diameter is 5-meters, with nine of the Thunder R-1 engines to power the first-stage.
Flight profile involves a reusable first-stage returning to land on an offshore platform after main engine cut-off. Company marketing materials portray the offshore platform as similar to an oil platform.
