NII Mash N2O4/UDMH rocket engine. Almaz, Kvant, Kristall, Spektr, Priroda. In Production. Low-thrust attitude control thruster. Used in Isayev 11D458 engine.
AKA: 11D458. Status: In Production. Thrust: 400 N (80 lbf). Unfuelled mass: 2.50 kg (5.50 lb). Specific impulse: 255 s.
Engine: 2.50 kg (5.50 lb). Chamber Pressure: 9.00 bar. Thrust to Weight Ratio: 16.4.
Family:
Storable liquid.
Country:
Russia.
Propellants:
N2O4/UDMH.
Stages:
Proton KM-4 Briz M,
Rokot-3 Briz.
Agency:
NII Mash.
Bibliography:
336.