FIELD: mechanical engineering; draining propellant components from tanks of liquid propellant rocket launchers. SUBSTANCE: mass of liquid phase (A) of local accumulation of propellant component at lower point of hydraulic system settles on walls of tank in form of solid phase (B) after draining of near-wall layer from tank due to supply of heat Q1 and removal of heat Q2, thus creating unbalanced state of system, i.e. shifting the thermodynamic process in gaseous form (1) from area of boiling point to area of hardening point . EFFECT: enhanced efficiency. 4 dwg
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Authors
Dates
1997-05-10—Published
1993-11-01—Filed