Device for pressurizing propellant tanks of a rocket engine
The device comprises two heat exchangers ( 74, 90 ) suitable respectively for vaporizing first and second propellants before they are reintroduced in gaseous form into their tanks ( 16, 18 ). The heat exchangers co-operate respectively with first and second gas generators ( 60, 84 ) suitable for being fed with a mixture of propellants in order to produce combustion, the second gas generator ( 84 ) being suitable for being fed at least in part by the exhaust from the first gas generator ( 60 ).
1. A device for pressurizing fuel tanks of a rocket engine, the device comprising
a first heat exchanger for vaporizing a first propellant coming from a first tank prior to the vaporized first propellant being reintroduced into the first tank, and
a second heat exchanger for vaporizing a second propellant coming from a second tank prior to the vaporized second propellant being reintroduced into the second tank, the first and second heat exchangers co-operating respectively with a first gas generator and a second gas generator configured to be fed with a mixture of the first and second propellants in order to produce combustion exhaust, and the second gas generator being arranged to be fed at least in part by the combustion exhaust from the first gas generator,
said device further comprising a regenerative heat exchange circuit using the combustion heat from the rocket engine to vaporize the first propellant, referred to as the regenerated propellant,
the device being configured for setting up a first situation in which the first gas generator is fed by the first and second tanks, while a first tapping pipe to the first heat exchanger for vaporizing the first propellant is deactivated and a second tapping pipe to the second heat exchanger for vaporizing the second propellant is activated.
2. The device as claimed in claim 1 , wherein the first and second propellants feeding the gas generators are pressurized.
3. The device as claimed in claim 1 , including first and second motor-driven pumps respectively a first tank outlet and a second tank outlet.
4. The device as claimed in claim 1 , wherein, in the first situation, the second gas generator is fed solely by the combustion exhaust of the first gas generator.
5. The device as claimed in claim 1 , configured for setting up a second situation in which the first gas generator is fed by the first and second tanks, the second gas generator is fed by the combustion exhaust of the first gas generator and by the second tank, and the first tapping pipe of the first heat exchanger and the second tapping pipe of the second heat exchanger are activated.
6. The device as claimed in claim 1 , wherein the first gas generator is fed by a first feed pipe and by a second feed pipe respectively connected to the first and second tanks, while the second gas generator is fed firstly by an exhaust pipe of the first gas generator and secondly by a third feed pipe connected to the second tank.
7. The device as claimed in claim 6 , wherein the third feed pipe is a branch connection on the second feed pipe.
8. The device as claimed in claim 7 , wherein the third feed pipe is connected to the second feed pipe via a branch valve.
9. The device as claimed in claim 6 , wherein the first heat exchanger is configured to be fed by the first tapping pipe connected to the first feed pipe, and the second heat exchanger is configured to be fed by the second tapping pipe connected to the second feed pipe.
10. The device as claimed in claim 9 , wherein the first tapping pipe is connected to the first feed pipe via a tapping valve.
11. The device as claimed in claim 6 , wherein feed valves are arranged respectively in the first and second feed pipes.
12. The device as claimed in claim 2 , configured for setting up a second situation in which the first gas generator is fed by the first and second tanks, the second gas generator is fed by the combustion exhaust of the first gas generator and by the second tank, and the first tapping pipe of the first heat exchanger and the second tapping pipe of the second heat exchanger are activated.