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8D715P

8D715P is the Kosberg RD0108 LOX/kerosene liquid rocket engine developed by OKB-154 (JSC KBKhA) for the 11A57 Voskhod Block I third stage. KBKhA lists 30.38 tf vacuum thrust (normalized here to 297.9 kN), 326 s specific impulse, and production at Factory No. 154 (VMZ); NASA dates its first use to 1963. This historical model remains distinct from the RD-0109/8D719 engine used on the earlier Block Ye stage.

Identity

Aliases
8D715PRD-0108RD0108Kosberg 8D715PKosberg RD0108
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
8D715P
Status
historical

Details

Description
8D715P is the Kosberg RD0108 LOX/kerosene liquid rocket engine developed by OKB-154 (JSC KBKhA) for the 11A57 Voskhod Block I third stage. KBKhA lists 30.38 tf vacuum thrust (normalized here to 297.9 kN), 326 s specific impulse, and production at Factory No. 154 (VMZ); NASA dates its first use to 1963. This historical model remains distinct from the RD-0109/8D719 engine used on the earlier Block Ye stage.
Developers
Manufacturers
Propellants
liquid oxygenkerosene
Rocket Specs
Cycle
gas-generator
Vacuum Specific Impulse S
326
Vacuum Thrust Kn
297.9

Links

Assets & Meta

Creation Time
July 29, 2026 at 08:05:02 UTC
Updated Time
August 23, 2026 at 01:40:53 UTC

Other

Sources