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RD-275

RD-275 is the uprated Proton first-stage variant directly modified from RD-253, using nitrogen tetroxide/UDMH propellants and the inherited oxidizer-rich staged-combustion architecture. Proton-PM records production beginning in 1992 and states that RD-275 was 7.7% more powerful than RD-253; the exact model is historical and retired, preceding the later RD-276.

Identity

Aliases
14D14
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-275
Status
retired

Details

Description
RD-275 is the uprated Proton first-stage variant directly modified from RD-253, using nitrogen tetroxide/UDMH propellants and the inherited oxidizer-rich staged-combustion architecture. Proton-PM records production beginning in 1992 and states that RD-275 was 7.7% more powerful than RD-253; the exact model is historical and retired, preceding the later RD-276.
Developers
Family
Lineage
  • Note
    Proton-PM records RD-275 as the next serial modification of RD-253, with thrust increased by 7.7 percent.
    Related Propulsion System
    Relationship
    direct-derivative-of
    Sources
Manufacturers
Propellants
nitrogen tetroxideUDMH
Rocket Specs
Cycle
oxidizer-rich staged combustion
Service Entry Date
1995

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:57:55 UTC
Updated Time
August 23, 2026 at 18:48:53 UTC

Other

Sources