CATALYTIC DECOMPOSITION REACTORS
A catalyst bed includes a structure defining a plurality of channels configured to receive flow of fluid to be chemically catalyzed. The plurality of channels are oriented at least partially non-parallel to an overall flow direction of the flow from inputs of the plurality of channels to outputs of the plurality of channels. A catalyst is exposed at an exterior of the structure.
1 . A method comprising:
atomizing a flow of a decomposable fluid to produce a spray of the decomposable fluid;
heating the spray of the decomposable fluid; and
chemically catalyzing a decomposition reaction of the heated spray of the decomposable fluid to produce two or more gaseous decomposition products.
2 . The method of claim 1 , comprising:
monitoring a temperature of a catalyst bed during thermal decomposition of the heated spray of the decomposable fluid; and
in response to determining that the temperature of the catalyst bed satisfies a condition, adjusting at least one of an intensity at which the spray of the decomposable fluid is heated or a flow rate of the decomposable fluid.
3 . The method of claim 1 , comprising:
directing at least one of the two or more gaseous decomposition products into a port of a solid fuel grain mass.
4 . The method of claim 3 , wherein the at least one of the two or more gaseous decomposition products comprises oxygen gas, and
wherein the method comprises causing combustion of the oxygen gas and the solid fuel grain mass.
5 . The method of claim 4 , comprising:
after initiation of the combustion, directing flow of the decomposable fluid into the port of the solid fuel grain mass through a flow path that bypasses a catalyst bed in which the decomposition reaction occurs.
6 . The method of claim 1 , comprising ejecting at least one of the two or more gaseous decomposition products out of a nozzle so as to produce thrust.
7 . The method of claim 1 , comprising:
providing at least one of pressure or heat to a pressure system component using at least one of the two or more gaseous decomposition products.
8 . The method of claim 7 , comprising providing the heat to the pressure system component by flowing the at least one of the two or more gaseous decomposition products through a heat exchanger that is thermally coupled to the pressure system component.
9 . The method of claim 7 , comprising providing the pressure to the pressure system component by injecting the at least one of the two or more gaseous decomposition products into the pressure system component.
10 . The method of claim 9 , comprising:
separating a first gaseous decomposition product of the two or more gaseous decomposition products from a second gaseous decomposition product of the two or more gaseous decomposition products; and
injecting the first gaseous decomposition product into the pressure system component.
11 . The method of claim 10 , wherein the first gaseous decomposition product comprises oxygen.
12 . The method of claim 7 , wherein the flow of the decomposable fluid originates at a tank, and wherein the pressure system component comprises the tank, a valve, a fluid line, or a pressure regulator.
13 . The method of claim 1 , wherein the decomposable fluid comprises nitrous oxide.
14 . The method of claim 1 , comprising jump-starting a turbine using at least one of the two or more gaseous decomposition products.
15 . A vehicle comprising:
a tank for storing a decomposable fluid;
a primary catalyst bed fluidically coupled to the tank;
a secondary catalyst bed fluidically coupled to the tank; and
a combustion chamber comprising a solid fuel grain mass, the combustion chamber fluidically coupled to an output of the primary catalyst bed.
16 . The vehicle of claim 15 , wherein the secondary catalyst bed has a smaller thermal mass than the primary catalyst bed.
17 . The vehicle of claim 15 , comprising a flow path coupling the tank to the combustion chamber, wherein the flow path bypasses the primary catalyst bed.
18 . The vehicle of claim 15 , comprising a coupling component fluidically coupled to an output of the secondary catalyst bed,
wherein the coupling component is configured to provide at least one of pressure or heat to a pressure system component using at least one gaseous decomposition product resulting from decomposition of the decomposable fluid at the secondary catalyst bed.
19 . The vehicle of claim 18 , wherein the coupling component comprises a heat exchanger that is arranged to thermally couple the pressure system component to the at least one gaseous decomposition product.
20 . The vehicle of claim 18 , wherein the coupling component comprises an injector arranged to inject the gaseous decomposition product into the pressure system component.
21 . The vehicle of claim 20 , comprising a gas separator configured to separate a first gaseous decomposition product of the at least one gaseous decomposition product from a second gaseous decomposition product of the at least one gaseous decomposition product, and to direct the first gaseous decomposition product into the injector.
22 . The vehicle of claim 21 , wherein the first gaseous decomposition product comprises oxygen gas.
23 . The vehicle of claim 18 , wherein the pressure system component comprises the tank, a valve, a fluid line, or a pressure regulator.
24 . The vehicle of claim 15 , comprising a nozzle fluidically coupled to an output of the secondary catalyst bed, the nozzle configured to produce thrust by ejection of at least one gaseous decomposition product resulting from decomposition of the decomposable fluid at the secondary catalyst bed.
25 . The vehicle of claim 15 , comprising a second combustion chamber fluidically coupled to an output of the secondary catalyst bed or the output of the primary catalyst bed.
26 . The vehicle of claim 25 , wherein the second combustion chamber has a dual-endburning configuration.
27 . The vehicle of claim 25 , comprising one or more nozzles configured to eject combustion products from combustion in the second combustion chamber.
28 . The vehicle of claim 15 , comprising a gas accumulator coupled to an output of the secondary catalyst bed, the gas accumulator configured to store at least one gaseous decomposition product resulting from decomposition of the decomposable fluid at the secondary catalyst bed.
29 . The vehicle of claim 15 , wherein the vehicle is a missile, a rocket, a plane, or a spacecraft.
30 . The vehicle of claim 15 , wherein the solid fuel grain mass defines a port, and wherein the vehicle comprises a flow path fluidically coupling an output of the primary catalyst bed to the port.
31 . The vehicle of claim 30 , comprising a nozzle in fluidic communication with the port, the nozzle configured to generate thrust by ejection of combustion products from the port.
32 . A catalyzing reactor system comprising:
a tank for storing a decomposable fluid;
a catalyst bed fluidically coupled to the tank;
an effervescent injector comprising
a gas flow channel,
a liquid flow channel, and
one or more orifices between the gas flow channel and the liquid flow channel,
wherein the gas flow channel is fluidically coupled to an output of the catalyst bed and is configured to receive at least one gaseous decomposition product resulting from catalytic decomposition of the decomposable fluid at the catalyst bed,
wherein the liquid flow channel is fluidically coupled to the tank and is configured to receive the decomposable fluid from the tank, and
wherein the one or more orifices are configured such that the at least one gaseous decomposition product flows from the gas flow channel into the liquid flow channel and aerates the decomposable fluid; and
a combustion chamber fluidically coupled to an output of the liquid flow channel.