FIELD: space engineering; transport spacecraft for topping-up orbital stations, type MIR in space. SUBSTANCE: according to invention, replenishment compartment includes oxidizer and fuel tanks with respective fittings and pressurization systems. Compartment is provided with inner cylindrical shell secured to housing by means of partitions which divide compartment into sectors so that oxidizer and fuel tanks together with their fittings and pressurization systems are arranged in diametrically opposite sectors. Provision is made to exclude formation of explosive mixture during operation even though in case of microleaks of propellent components. EFFECT: high fire safety and explosion proofness; enhanced reliability in topping-up tanks with self-inflammable components of propellant. 2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TOPPING-UP COMPONENTS COMPARTMENT | 1997 |
|
RU2116227C1 |
| PROPELLANT COMPARTMENT OF TRANSPORT SPACECRAFT | 2001 |
|
RU2196083C1 |
| PROPELLANT COMPARTMENT OF TRANSPORT SPACECRAFT | 2001 |
|
RU2196082C1 |
| REFILLING COMPONENT COMPARTMENT | 2001 |
|
RU2200119C1 |
| COMPARTMENT FOR COMPONENTS OF RECHARGING | 2001 |
|
RU2217359C2 |
| ON-BOARD COMPLEX OF CARGO SPACECRAFT | 2001 |
|
RU2208560C1 |
| COMPARTMENT FOR REPLENISHING COMPONENTS | 2003 |
|
RU2247685C1 |
| PROPELLANT MODULE | 2004 |
|
RU2270144C2 |
| COMPARTMENT FOR TOPPING-UP (REPLENISHMENT) COMPONENTS | 2003 |
|
RU2246430C1 |
| ANDROGYNOUS PERIPHERAL MATING UNIT AND DAMPER OF SHOCK-ABSORBING AND ACTUATING SYSTEM FOR THIS UNIT | 1998 |
|
RU2131829C1 |
