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RD-276

RD-276, formerly described as RD-275M/14D14M, is the final uprated Proton-M first-stage variant: a single-chamber nitrogen-tetroxide/UDMH engine using oxidizer-rich staged combustion. Proton-PM identifies it as a modernized RD-253/RD-275 derivative, records service from 2007, and reports its continued use on Proton-M launches in 2026.

Identity

Aliases
RD-275M14D14M
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-276
Status
active

Details

Description
RD-276, formerly described as RD-275M/14D14M, is the final uprated Proton-M first-stage variant: a single-chamber nitrogen-tetroxide/UDMH engine using oxidizer-rich staged combustion. Proton-PM identifies it as a modernized RD-253/RD-275 derivative, records service from 2007, and reports its continued use on Proton-M launches in 2026.
Developers
Family
Lineage
Manufacturers
Propellants
nitrogen tetroxideUDMH
Rocket Specs
Chamber Count
1
Cycle
oxidizer-rich staged combustion
Sea Level Specific Impulse
…
Sea Level Thrust
…
Vacuum Specific Impulse
…
Vacuum Thrust
…
Service Entry Date
2007

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:57:58 UTC
Updated Time
August 23, 2026 at 18:57:02 UTC

Other

Sources
RD-276 - AeroVia