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Engine Model: Atar 9K. Designer: SNECMA. Propellants: Air/Kerosene. Thrust(vac): 48.000 kN (10,790 lbf). Thrust(sl): 43.600 kN (9,802 lbf). Isp: 2,020 sec. Isp (sea level): 1,836 sec. Burn time: 15,000 sec. Chambers: 1. Country: France. Status: Out of Production.
Atar 9K used on Rocket Stages
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