Taurus-II rocket is designed for launchings under the U.S. government and NASA programs on commercial cargo delivery to the ISS for medium-class payloads.
YUZMASH produces the central unit of the first stage of Taurus-II launch vehicle. The stage diameter - 3.9 m.
|Maximum lift-off mass, t||290|
|Payload weight, t||over 5|
|Vacuum thrust, ts||310|
|Propulsion components||oxygen + kerosene|
|1,2 stage diameter, m||3,9|
|Fairing diameter, m||3,9|
|Number of stages||2 + orbital module|