FIELD: space engineering. SUBSTANCE: air supply has high-pressure compressed-air receivers communicating through reducer with feed pipeline. The latter communicates with space vehicle through thin- walled pipeline joined by means of on-board connector. Electric heater is made in the form of heat-insulating case filled with liquid antifreeze. Case accommodates coaxially mounted coils connected to feed pipeline; tubular electric heaters of different power are placed in annular gap between coils. The latter are made of stainless steel; ratio of outer diameters of turns of external and internal coils is 1.3-2.0; ratio of total length of coils to inner diameter of coil is between 2000 and 4000. EFFECT: provision for maintaining desired temperature of space vehicle. 2 cl, 3 dwg, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR THERMOSTATING OF SPACE OBJECTS | 2002 |
|
RU2215951C2 |
GEAR FOR AIR THERMOSTATIC CONTROL OVER SPACE OBJECTS | 2000 |
|
RU2184912C2 |
SPACE OBJECT AIR THERMOSTATTING SYSTEM | 2000 |
|
RU2190165C2 |
METHOD FOR THERMAL CONDITIONING OF SPACEHEAD BY HIGH PRESSURE AIR AND SYSTEM FOR ITS IMPLEMENTING | 2006 |
|
RU2335438C1 |
METHOD FOR THERMAL CONDITIONING OF SPACEHEAD BY HIGH PRESSURE GAS AND SYSTEM FOR ITS IMPLEMENTING | 2006 |
|
RU2335439C1 |
METHOD AND DEVICE FOR THERMOSTATIC CONTROL OF SPATIAL OBJECTS AND BOOSTER COMPARTMENTS | 2007 |
|
RU2335706C1 |
DEVICE FOR AIR CONDITIONING OF SPATIAL OBJECTS | 2007 |
|
RU2339554C1 |
LAUNCHING COMPLEX FOR PRE-LAUNCH PREPARATION AND LAUNCHING OF LAUNCH VEHICLE WITH SPACE NOSE CONE (VERSIONS) | 2006 |
|
RU2318706C1 |
DEVICE FOR AIR THERMOSTATTING OF SPACE OBJECTS | 2001 |
|
RU2201384C2 |
LAUNCH COMPLEX FOR PREPARATION AND LAUNCHING OF LAUNCH VEHICLES WITH SPACECRAFT | 2004 |
|
RU2270792C1 |
Authors
Dates
1999-08-27—Published
1998-01-05—Filed