Back to Propulsion Systems

RD-191

NPO Energomash RD-191 is a single-chamber liquid-oxygen/kerosene engine with oxidizer-rich staged combustion, developed for the Angara launch-vehicle family from the RD-170/RD-171 architecture. The NPO Energomash technical paper reports a nominal 196 metric-ton-force thrust level (approximately 1,922 kN) and describes a 2009 Universal Rocket Module firing of about 233 s, including throttling from 100% to 37.6% nominal thrust.

Identity

Aliases
RD-191РД-191NPO Energomash RD-191Angara RD-191
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
RD-191
Status
active

Details

Description
NPO Energomash RD-191 is a single-chamber liquid-oxygen/kerosene engine with oxidizer-rich staged combustion, developed for the Angara launch-vehicle family from the RD-170/RD-171 architecture. The NPO Energomash technical paper reports a nominal 196 metric-ton-force thrust level (approximately 1,922 kN) and describes a 2009 Universal Rocket Module firing of about 233 s, including throttling from 100% to 37.6% nominal thrust.
Developers
Family
Lineage
Manufacturers
Propellants
liquid oxygenkerosene
Rocket Specs
Chamber Count
1
Cycle
oxidizer-rich staged combustion
Sea Level Thrust Kn
1922.1

Links

Assets & Meta

Creation Time
July 29, 2026 at 09:56:28 UTC
Updated Time
August 22, 2026 at 07:36:22 UTC

Other

Sources