Initial Operational Capability (IOC):
Parent System: RD-169
Initial Operational Capability (IOC): 2000
Total Production: ?
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Description: The RD-169 is a rocket engine developed by Russia as part of the RD-120 engine family in the 1990s. Its development was completed in the early 2000s. The engine uses Liquefied Natural Gas (LNG) and Liquefied Oxygen (LOx) as fuel. The RD-169 has been selected as the second stage motor for the Soyuz-5 medium-weight space launch system.
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