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  • Thumbnail for Ọkọ̀-àlọbọ̀ Òfurufú
    LOX/LH2 Second stage - Orbiter Engines 2 OME Thrust 53.4 kN combined total vacuum thrust (12,000 lbf) Specific impulse 316 s Burn time 1250 s Fuel MMH/N2O4...
    3 KB (àwọn ọ̀rọ̀ 3) - 14:34, 1 Oṣù Èrèlé 2017