FIELD: space engineering; transport spacecraft for re-charging orbital stations, such as MIR. SUBSTANCE: spacecraft compartment has case with external heat insulation and framework mounted inside it. Fuel and oxidizer tanks provided with respective fittings, pipe lines and bottles of pressurization system are secured on framework. Framework is made in form of two cone-shaped envelopes connected by frame over larger base. Mounted in joint area is perforated circular partition fastening cone-shaped shells. Part of framework cavity between frame and circular partition is communicated with ground gas preheating and supply system by means of gas supply main. This gas is smoothly distributed in volume of compartment through perforations of partition and escapes through special holes and gaps. According to invention, provision is made for effective thermostatic control of propellant components contained in tanks under ground conditions in charging the spacecraft and during storage on launching position. EFFECT: enhanced strength of compartment. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ON-BOARD COMPLEX OF CARGO SPACECRAFT | 2001 |
|
RU2208560C1 |
PROPELLANT COMPARTMENT OF TRANSPORT SPACECRAFT | 2001 |
|
RU2196082C1 |
COMPARTMENT FOR COMPONENTS OF RECHARGING | 2001 |
|
RU2217359C2 |
ON-BOARD COMPLEX OF CARGO SPACECRAFT | 2001 |
|
RU2207308C1 |
REFILLING COMPONENT COMPARTMENT | 2001 |
|
RU2200119C1 |
PROPELLANT MODULE | 2004 |
|
RU2266241C1 |
COMPARTMENT FOR REPLENISHING COMPONENTS | 2003 |
|
RU2247685C1 |
ROCKET CRYOGENIC STAGE | 2000 |
|
RU2153447C1 |
COMPARTMENT FOR REPLENISHMENT COMPONENTS | 1998 |
|
RU2132804C1 |
COMPARTMENT FOR TOPPING-UP (REPLENISHMENT) COMPONENTS | 2003 |
|
RU2246430C1 |
Authors
Dates
2003-01-10—Published
2001-10-29—Filed