Izotov LK-700

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Izotov LK-700

Part of 8D423

Izotov N2O4/UDMH rocket engine. LK-700. Developed 1966-69.

Status: Developed 1966-69. Date: 1966-69. Thrust: 131.00 kN (29,449 lbf).

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Izotov bureau.

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