ISRO Semi-cryogenic Engine update

ISRO's Semi-cryo Engine illustration. (credit ISRO)

 ISRO's Semi-cryogenic Engine specifications are following:

• Thrust (vacuum) - 2000 kN
• Isp (vacuum) - 3285 N-s/kg
• Chamber Pressure - 18 MPa
• Mixture Ratio - 2.65
• Thrust Throttling - 65-105 (% of nominal thrust) 
• Engine gimbal - 8 degrees (in two planes)