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RD-108
© Photo by A. Sdobnikov / Wikimedia Commons / CC BY 3.0

RD-108

Core stage engine of the R-7

معروض
The RD-108 differs from its strap-on sibling in having more vernier chambers — four instead of two — and a tuning for longer operation: the core stage keeps accelerating after the boosters separate, so the nozzles are optimised for thinner air. A cluster of one RD-108 and four RD-107s gives about 4 meganewtons of thrust at lift-off. All twenty chambers ignite simultaneously on the ground: in-flight ignition of such a cluster would be an unjustified risk. On display is a sectioned engine showing the turbopump assembly, the gas generator and the chamber cooling passages.

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