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.