STAND FOR AMMONIA FILLING AND PROCESS OF FILLING OF ACTIVE DOUBLE-PHASE SYSTEM OF THERMAL CONTROL OF SPACECRAFT WITH AMMONIA Russian patent published in 2003 - IPC

Abstract RU 2200307 C2

FIELD: equipment and technology for tightness testing. SUBSTANCE: proposed stand has filling and vent valves and tank with ammonia. Outlet of tank is linked to compressor which outlet communicates through connection main lines to filling valves of system of thermal control. There are provided high-vacuum pump unit, units for analysis of residual uncondensed gases, for ammonia circulation, for measurement of lack of tightness in mentioned valves, in system of thermal control and in connection main lines, units feeding helium, nitrogen, drain lines and control devices. Proper outlets and inlets of above-mentioned units, main and drain lines communicate through cut-off valves to filling and vent valves of system of thermal control. In accordance with proposed process system of thermal control is vacuumed together with connection main lines, units for analysis and circulation to ≤10-2 mm Hg and specified amount of liquid ammonia is fed into it. Value of air inleakage from outside is measured and if it is less than permissible value vacuum pumping and ammonia circulation are continued in system of thermal control and connection main lines for required number of times till equilibrium concentration of residual uncondensed gases is achieved. Draining and filling with ammonia of system of thermal control and communication main lines alternate while measuring impurities in these gases. If no given impurities are detected then system of thermal control and communication main lines filled with ammonia are shut off, ammonia is drained and communication main lines are vacuumed. Growth of pressure with evaporation of ammonia in communication main lines is controlled and if value of measured pressure increase is less than permissible value communication main lines are filled with dry nitrogen and are disconnected from system of thermal control. EFFECT: enhanced reliability of filling of system of thermal control by way of reduction of share of residual uncondensed gases in it. 3 cl, 1 dwg

Similar patents RU2200307C2

Title Year Author Number
METHOD OF FILLING HYDRAULIC SYSTEMS OF TEMPERATURE CONTROL SYSTEMS OF SPACECRAFT WITH HEAT-TRANSFER AGENT 2001
  • Tsikhotskij V.M.
RU2196711C2
METHOD OF FILLING SPACECRAFT HYDRAULIC TEMPERATURE CONTROL SYSTEM EQUIPPED WITH HYDROPNEUMATIC COMPENSATOR WITH HEAT-TRANSFER AGENT AND DEVICE FOR REALIZATION OF THIS METHOD 2003
  • Tsikhotskij V.M.
RU2252901C1
METHOD OF FILLING OF FLUID CIRCUIT HYDRAULIC LINE WITH WORKING FLUID EQUIPPED WITH HYDROPNEUMATIC COMPENSATOR OF WORKING FLUID VOLUME EXPANSION 2012
  • Tsikhotskij Vladislav Mikhajlovich
RU2509695C1
METHOD OF FILLING HYDRAULIC LINES OF PAYLOAD DELIVERED BY SPACE OBJECTS WITH PROPULSIVE MASS 2004
  • Tsikhotskij Vladislav Mikhajlovich
RU2271969C2
DEVICE TO COMPENSATE FOR LOSSES OF WORKING MEDIUM FROM HYDRAULIC MAIN LINE OF SEALED MANNED COMPARTMENT THERMAL CONTROL SYSTEM AND METHOD OF ITS OPERATION 2012
  • Tsikhotskij Vladislav Mikhajlovich
RU2497731C1
DEVICE FOR WORKING MEDIUM IN-FLIGHT REFILLING OF HYDRAULIC PIPELINE OF SPACECRAFT THERMOREGULATION SYSTEM EQUIPPED WITH HYDRO PNEUMATIC COMPENSATOR OF VOLUME EXPANSION OF WORKING MEDIUM, AND METHOD OF OPERATION OF THIS DEVICE 2006
  • Tsikhotskij Vladislav Mikhajlovich
RU2324629C2
DEVICE FOR FILLING SPACECRAFT TEMPERATURE CONTROL SYSTEM WITH LIQUID HEAT-TRANSFER AGENT 2006
  • Bezrukikh Aleksej Dmitrievich
  • Fedorycheva Irina Valentinovna
RU2317925C1
METHOD OF AND DEVICE FOR FILLING VEHICLE FUEL SYSTEMS 2002
  • Cheljaev V.F.
RU2220062C2
CRYOGENIC VESSEL FILLING METHOD AND SYSTEM 2002
  • Gorelikov V.I.
RU2221965C2
METHOD FOR SPACECRAFT TEMPERATURE CONTROL HYDRAULIC SYSTEM FILLING WITH COOLANT 2007
  • Tsikhotskij Vladislav Mikhajlovich
RU2356804C1

RU 2 200 307 C2

Authors

Lipnjak L.V.

Prokhorov Ju.M.

Trojnikov V.I.

Tsikhotskij V.M.

Shcherbakov Eh.V.

Dates

2003-03-10Published

2001-02-13Filed