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Proton (UR-500)

The original UR-500, later named Proton, was the two-stage first configuration of the Soviet heavy launch vehicle. Its 1965–1966 flight-test program launched the Proton 1, Proton 2, and Proton 3 scientific satellites and established the clustered hypergolic architecture from which the three-stage Proton-K was developed.

Proton (UR-500)
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Identity

Aliases
UR-5008K82Two-stage Proton
Family Name
Proton
Full Name
Proton (UR-500)
Status
retired
Type
rocket
Variant Name
UR-500

Details

Description
The original UR-500, later named Proton, was the two-stage first configuration of the Soviet heavy launch vehicle. Its 1965–1966 flight-test program launched the Proton 1, Proton 2, and Proton 3 scientific satellites and established the clustered hypergolic architecture from which the three-stage Proton-K was developed.
First Flight Year
1,965
Last Flight Year
1,966
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Nested value
    • Nested value
    Name
    UR-500 (8K82) original two-stage configuration
    Notes
    Exact original Proton second-stage engine block documented by KBKhA: three RD-0208 main engines plus one RD-0209 tank-pressurization companion engine.
Rocket Specs
Reusability
expendable
Stages Count
2

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Assets & Meta

Creation Time
July 14, 2026 at 17:02:26 UTC
Updated Time
August 15, 2026 at 17:41:34 UTC

Other

Search Name
Proton (UR-500) UR-500 8K82 Two-stage Proton