FIELD: space engineering; servicing orbital stations, type MIR in space.
SUBSTANCE: proposed compartment has housing and oxidizer and fuel tanks secured on its frame and provided with fittings and supercharging system. Tanks with different components are combined in propellant modules which are diametrically opposite relative to each other. Compartment includes additionally oxygen bottles and water reservoirs mounted on said frame between propellant modules diametrically opposite relative to each other. Provision is made for electric heaters made from carbon cloth and located mainly in zones of water reservoirs. Outer surfaces of fuel and oxidizer tanks, oxygen bottles and water reservoirs and inner surface of housing are covered with temperature control coats. Outer surface of housing is coated with heat insulation.
EFFECT: simplified centering of compartment due to effective thermostatting of units located in this compartment.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PROPELLANT MODULE | 2004 |
|
RU2270144C2 |
| COMPARTMENT OF REFUELING COMPONENTS | 2003 |
|
RU2276044C2 |
| PROPELLANT MODULE | 2004 |
|
RU2266241C1 |
| PROPELLANT COMPARTMENT OF TRANSPORT SPACECRAFT | 2001 |
|
RU2196082C1 |
| ON-BOARD COMPLEX OF CARGO SPACECRAFT | 2001 |
|
RU2208560C1 |
| COMPARTMENT FOR REPLENISHMENT COMPONENTS | 1998 |
|
RU2132804C1 |
| COMPARTMENT FOR REPLENISHING COMPONENTS | 2003 |
|
RU2247685C1 |
| TOPPING-UP COMPONENTS COMPARTMENT | 1997 |
|
RU2116227C1 |
| PROPELLANT COMPARTMENT OF TRANSPORT SPACECRAFT | 2001 |
|
RU2196083C1 |
| REFILLING COMPONENT COMPARTMENT | 2001 |
|
RU2200119C1 |
