A combined launch vehicle and satellite system
US-2024051685-A1 · Feb 15, 2024 · US
US2017073089A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017073089-A1 |
| Application number | US-201515310419-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 11, 2015 |
| Priority date | May 13, 2014 |
| Publication date | Mar 16, 2017 |
| Grant date | — |
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A vapor jet system to continuously jet vapors while suppressing cavitation. One vapor jet system includes a liquid storage part for separately storing two or more kinds of mutually insoluble liquids; a jet orifice; and a jet control part. Jetting the vapors is from a state where pressure in the space storing the vapors in the liquid storage part is higher than the saturated vapor pressure in any of the two or more kinds of liquids. Alternatively, a vapor jet system can include a fluid storage part storing one kind of liquid and at least one kind of inactive gas having a composition different from the liquid; a similar jet orifice; and a similar jet control part. Jetting the vapors and inactive gas(es) is (are) from a state where pressure in a vapor storing space in the fluid storage part is higher than the saturated vapor pressure in the liquid.
Opening claim text (preview).
1 . A vapor jet system comprising: a liquid storage part for separately storing two or more kinds of mutually insoluble liquids; a jet orifice for jetting out vapors generated by vaporization of the two or more kinds of liquids inside of the liquid storage part; and a jet control part for controlling the jetting out of the vapors from the jet orifice, wherein the system is configured to start jetting out of the vapors from a state where the pressure in the space storing the vapors in the liquid storage part is higher than the saturated vapor pressure in any of the two or more kinds of liquids. 2 . The vapor jet system according to claim 1 , wherein the two or more kinds of mutually insoluble liquids are liquid ammonia or ammonia water and liquid butane. 3 . The vapor jet system according to claim 1 , further comprising heaters for heating the liquid storage part. 4 . The vapor jet system according to claim 1 , wherein the liquid storage part further comprise two or more liquid holding members for holding each one of the two or more kinds of liquids. 5 . A vapor jet system comprising: a fluid storage part storing one kind of liquid and at least one kind of inactive gas having a composition different from the liquid; a jet orifice for jetting out vapors generated by vaporization of the liquid inside of the fluid storage part and the at least one kind of inactive gas; and a jet control part for controlling the jetting out of the vapors and the at least one kind of inactive gas from the jet orifice, wherein the system is configured to start jetting out of the vapors and the at least one kind of inactive gas from a state where the pressure in the space storing the vapors in the fluid storage part is higher than the saturated vapor pressure in the liquid. 6 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 1 . 7 . The vapor jet system according to claim 2 , further comprising heaters for heating the liquid storage part. 8 . The vapor jet system according to claim 2 , wherein the liquid storage part further comprise two or more liquid holding members for holding each one of the two or more kinds of liquids. 9 . The vapor jet system according to claim 3 , wherein the liquid storage part further comprise two or more liquid holding members for holding each one of the two or more kinds of liquids. 10 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 2 . 11 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 3 . 12 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 4 . 13 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 5 . 14 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 7 . 15 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 8 . 16 . A thruster configured to obtain thrust force by jetting out the vapors from the jet orifice using the vapor jet system according to claim 9 .
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