FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and can be used for temperature regulation of a lunar rocket launching complex (LLC). LLC heating system has a fluid loop, a heat carrier, a thermal casing with thermal accumulators and a sliding cover with an automatic opening/closing system with light sensors, a pump station, a heating control system, solar batteries and an electric accumulator. One half of the thermal accumulators are filled with the liquid heat carrier, and another one is empty. The thermal casing contains the external smooth surface and an internal surface covered with a heat-insulating material (teflon, polytetrafluoroethylene, polychlorotrifluoroethylene, crystal copolymer of ethylene with tetrafluoroethylene).
EFFECT: invention allows improving the reliability of LLC thermal control.
5 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF HEATING THE LUNAR ROCKET LAUNCHER COMPLEX | 2012 |
|
RU2511746C2 |
| MOON LAUNCH MISSILE SYSTEM | 2012 |
|
RU2518377C2 |
| CONTROL SUPPORT CENTRE FOR ASTEROIDAL SAFETY SYSTEM | 2012 |
|
RU2518504C2 |
| THERMOSTATING SYSTEM FOR CRYOGENIC FUEL COMPONENTS OF AN ENCAPSULATED SILO-BASED ROCKET | 2022 |
|
RU2809671C2 |
| METHOD OF CONTROL OF TEMPERATURE OF HEAT- TRANSFER AGENT IN TEMPERATURE CONTROL SYSTEM OF SPACECRAFT WITH RADIATING RADIATOR | 2000 |
|
RU2187083C2 |
| OFF-LINE SURVIVAL SYSTEM | 2002 |
|
RU2215244C1 |
| METHOD OF ACCUMULATING SPACESHIP POWER SUPPLY | 2010 |
|
RU2451631C1 |
| METHOD OF SPACECRAFT TEMPERATURE CONTROL | 2003 |
|
RU2262469C2 |
| UNIVERSAL SPACE ROCKET SYSTEM FOR HIGH-CAPACITY TRANSPORT SYSTEMS | 2023 |
|
RU2811792C1 |
| WATER PRODUCER ON THE MOON | 2021 |
|
RU2770385C1 |
