Q12379762: Difference between revisions
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{{Page|11D458|Classes|Isayev N2O4/UDMH rocket engine. 0.392 kN. In Production. Isp=252s. Small attitude control thruster in Briz upper stage}} | {{Page|11D458|Classes|Isayev N2O4/UDMH rocket engine. 0.392 kN. In Production. Isp=252s. Small attitude control thruster in Briz upper stage|}} |
Latest revision as of 22:37, 22 February 2025
Isayev N2O4/UDMH rocket engine. 0.392 kN. In Production. Isp=252s. Small attitude control thruster in Briz upper stage.
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