FIELD: rocket engines. SUBSTANCE: according to proposed method working steam for operation of turbine is obtained from water using heat of rocket propellant combustion products. Steam is operated to pressure of 0.6-4.0 MPa. Used steam is cooled using cold of oxidizer and condensate is returned into water pump. EFFECT: prevention of freezing of water condensate at high pressure level in chamber. 2 dwg
Authors
Dates
2003-09-10—Published
2002-02-21—Filed