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Featured Image (Credits ISRO)

Thursday, June 20, 2013

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)


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