FIELD: astronautics.
SUBSTANCE: invention relates to the devices for thermostating of the spacecraft (SC) in case of its various (electrical, radio engineering, etc.) ground tests. Offered means are made in the form of a modular design – thermostatic control panels containing air ducts, which are fixed on the technological equipment (3), including collectors (2) and air distributors (4) over the surface (7) of the panelized SC. Inputs (1) of the collectors (2) are hermetically connected to the air-conditioning unit (not shown), and the outputs (5) – with the inputs of the distributors (4), which have parallel branched circuits with nozzles (6). Nozzles are equipped with removable chokes to adjust the air flow. During thermostat control of the SC, a number of nozzles (6) can be closed with covers.
EFFECT: technical result consists in reducing the required flow of thermostating air, as well as in unifying the means of its distribution and supplying to the surface of the SC.
1 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF AIR THERMAL CONDITIONING OF SPACE VEHICLE MODULES DURING GROUND TESTING AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2657603C1 |
METHOD FOR AIR TEMPERATURE CONTROL OF AUTONOMOUS BLOCKS OF SPACECRAFT DURING GROUND TESTS USING A RADIATOR AND AN AERODYNAMIC MODULE FOR ITS IMPLEMENTATION | 2022 |
|
RU2778102C1 |
DEVICE FOR THERMAL CONDITIONING OF ONBOARD DEVICES OF SPACE VEHICLE LOCATED IN ASSEMBLING-PROTECTION BLOCK OF SPACE ROCKET (VERSIONS) | 2013 |
|
RU2570849C2 |
SPACECRAFT EQUIPMENT THERMAL CONTROL SYSTEM | 2012 |
|
RU2494933C1 |
DEVICE TO CONTROL THERMAL CONDITIONS AND CLEANLINESS OF SPACECRAFT HEAD WITH LARGE-SIZED PAYLOAD | 2014 |
|
RU2557092C1 |
METHOD OF SPACECRAFT TEMPERATURE CONTROL | 2003 |
|
RU2262469C2 |
DEVICE FOR REMOVING AEROSOL POLLUTANTS FROM AMBIENT AIR | 2009 |
|
RU2390759C1 |
SPACE OBJECT TEMPERATURE CONTROL SYSTEM | 2002 |
|
RU2216490C1 |
METHOD AND DEVICE FOR THERMOSTATIC CONTROL OF SPATIAL OBJECTS AND BOOSTER COMPARTMENTS | 2007 |
|
RU2335706C1 |
METHOD FOR THERMOSTATTING PAY LOAD AND INSTRUMENTS OF CONTROL SYSTEM OF SPACE HEAD OF CARRIER ROCKET, AND AIRBORNE SYSTEM USED FOR METHOD REALISATION | 2007 |
|
RU2353556C2 |
Authors
Dates
2018-11-22—Published
2017-07-11—Filed