Back to Propulsion Systems

YF-102RV

YF-102RV is the high-altitude open-cycle liquid-oxygen/kerosene derivative of YF-102 for the Long March 12B second stage. China Aerospace Science and Technology Corporation describes one YF-102RV operating in the second stage, inheriting the core YF-102 technology while adapting the engine for near-vacuum operation with pump-front gimbal and a large-area-ratio nozzle. This exact propulsion record does not infer unsupported thrust or specific-impulse figures.

Identity

Aliases
YF-102RVYF102RVYF-102RV high-altitude rocket engineCASC YF-102RV
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
YF-102RV
Status
active

Details

Description
YF-102RV is the high-altitude open-cycle liquid-oxygen/kerosene derivative of YF-102 for the Long March 12B second stage. China Aerospace Science and Technology Corporation describes one YF-102RV operating in the second stage, inheriting the core YF-102 technology while adapting the engine for near-vacuum operation with pump-front gimbal and a large-area-ratio nozzle. This exact propulsion record does not infer unsupported thrust or specific-impulse figures.
Propellants
liquid oxygenkerosene
Rocket Specs
Cycle
open cycle

Links

Assets & Meta

Creation Time
August 14, 2026 at 00:30:13 UTC
Updated Time
August 23, 2026 at 17:52:30 UTC

Other

Sources
  • Accessed Date
    2026-08-13
    Note
    CASC specifies one YF-102RV high-altitude LOX/kerosene engine on Long March 12B second stage.
    Publisher
    China Aerospace Science and Technology Corporation
    Title
    Long March 12B launches constellation satellites
  • Accessed Date
    2026-08-13
    Note
    CNSA describes the YF-102V high-altitude derivative as inheriting the YF-102 technology base; the Long March 12B source identifies the RV variant.
    Publisher
    China National Space Administration
    Title
    China releases three commercial liquid rocket engines
  • Accessed Date
    2026-08-23
    Note
    CASC distinguishes the second-stage YF-102RV from the first-stage YF-102R and describes the high-altitude variant as using pump-front gimbal and a large-area-ratio nozzle for near-vacuum operation.
    Publisher
    China Aerospace Science and Technology Corporation
    Title
    In-depth interpretation of the Long March 12B launch vehicle