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Vostok-2M (8A92M) Launch Vehicle

Vostok-2M (8A92M) was a three-stage Soviet orbital launch vehicle in the R-7 lineage, used from 1964 through 1991. Developed as a specialized successor to Vostok-2, it placed Meteor weather, Tselina-D signals-intelligence, Resurs Earth-observation, Interkosmos, and Indian IRS spacecraft into high-inclination and Sun-synchronous orbits.

Vostok-2M (8A92M) Launch Vehicle
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Identity

Aliases
Vostok 8A92M8A92MVostok-MVostok-M 8A92M
Family Name
Vostok-2M
Full Name
Vostok-2M (8A92M) Launch Vehicle
Status
retired
Type
rocket

Details

Description
Vostok-2M (8A92M) was a three-stage Soviet orbital launch vehicle in the R-7 lineage, used from 1964 through 1991. Developed as a specialized successor to Vostok-2, it placed Meteor weather, Tselina-D signals-intelligence, Resurs Earth-observation, Interkosmos, and Indian IRS spacecraft into high-inclination and Sun-synchronous orbits.
Dimensions
Diameter M
2.95
Height M
38.8
First Flight Year
1,964
Last Flight Year
1,991
Manufacturer
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Nested value
    • Nested value
    • Nested value
    Name
    Vostok-2M 8A92M configuration
    Notes
    Exact three-stage Vostok-2M stack: four RD-107 booster engines, one RD-108 core engine, and one RD-0109 Block E engine. Vostok-2M lower-stage production suffixes evolved during its long service life; no narrower 8D74K/8D75K or later suffix is asserted without a canonical variant record.
Rocket Specs
Liftoff Mass Kg
283,100
Reusability
expendable
Stages Count
3
Strap On Boosters Count
4

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Creation Time
July 18, 2026 at 21:57:24 UTC
Updated Time
August 1, 2026 at 14:33:16 UTC

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Vostok-2M (8A92M) Launch Vehicle Vostok 8A92M 8A92M Vostok-M Vostok-M 8A92M