Status: Out of Production. Date: 1953-59. Thrust: 93.00 kN (20,907 lbf). Specific impulse: 218 s. Specific impulse sea level: 218 s.
Propellant Formulation: AK20I/T-1. Oxidizer to Fuel Ratio: 3.76.
Family: Storable liquid. Country: Russia. Launch Vehicles: R-11FM. Propellants: Nitric acid/Kerosene. Agency: Isayev bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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