US3135703A - Thrust chamber catalyst structure - Google Patents
Thrust chamber catalyst structure Download PDFInfo
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- US3135703A US3135703A US841173A US84117359A US3135703A US 3135703 A US3135703 A US 3135703A US 841173 A US841173 A US 841173A US 84117359 A US84117359 A US 84117359A US 3135703 A US3135703 A US 3135703A
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- catalyst
- silver
- thrust chamber
- catalyst bed
- nickel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01J—CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY; THEIR RELEVANT APPARATUS
- B01J23/00—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00
- B01J23/70—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper
- B01J23/89—Catalysts comprising metals or metal oxides or hydroxides, not provided for in group B01J21/00 of the iron group metals or copper combined with noble metals
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
- C06D5/04—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by auto-decomposition of single substances
Definitions
- This invention relates to improvements in monopropellent thrust chambers, and more particularly to an im proved catalyst bed device in a thrust chamber using 90% hydrogen peroxide as the propellent, for employment for example to provide attitude control effects in high altitude or space vehicles.
- the catalyst component is of particular importance; and various catalyst configurations have been previously used with a view to obtaining acceptable operation.
- porous porcelain stones impregnated with calcium, potassium, or sodium permanganate have I been used.
- silver metal strips in various shapes and configurations have been employed; the silver sometimes being treated with samarium nitrate to increase its catalytic activity.
- Platinum has also been used as the catalyst metal; each catalyst metal and/or configuration having been previously designed to obtain maximum specific impulse and eiciency of the propellent use.
- a more specific object is to provide an improved catalyst bed as aforesaid which comprises a porous bed of catalyst metal parts having surface characteristics resulting in improved gas-evolution.
- Another object is to provide an improved catalyst bed as aforesaid providing greatly improved response time, due to an improved surface area-to-volume ratio.
- Still another object is to provide an improved catalyst with one form of a catalyst bed construction of the present invention.
- FIG. 2 is a sectional view through a detail of the catalyst bed component thereof.
- FIG. 3 is an enlarged scale schematic sectional view illustrating the form of the catalyst metal construction.
- the invention is employed in conjunction with a rocket engine comprising generally a thrust chamber 10, which is of conventional form and includes a mounting flange portion 12; a catalyst bed chamber 14; and a thrust nozzle portion 16; it being understood that the present invention may be employed in conjunction with a thrust chamber of any other suitable design in lieu of the thrust chamber conguration shown in FIG. 1.
- the hydrogen peroxide inlet port' is indicated at 18, and a dispersion plate vis provided as indicated at 20 to distribute the hydrogen peroxide uniformly throughout the cross section of the catalyst chamber 14.
- a perforate holding or blast dispersion plate 22 is provided to retain the catalyst bed in operative position while permitting the evolving gases to exit to the thrust nozzle 16.
- each disc 28 comprises a wire mesh fabrication of transversely woven nickel wire strands 30-30. It 'is a particular feature of the present invention that each wire mesh disc fabrication as shown herein comprises a basis metal fabrication of nickel wire strands 30 which are subsequently plated with silver-gold alloy layers as indicated at 32 (FIG. 3).
- a nickel Wire screen member as a basis for the silver-gold valloy platings thereon, provides improved rigidity and heat resistant .characteristics for the overall structure, whereby the catalyst bed will be of improved overall resistance to fusing and/or attrition.
- the silver-gold alloy platings thereon provide optimum bed as aforesaid wherein the catalyst-surfaces are proas to provide improved rigidity of the bed, and improved resistance to fusing and attrition such as normally occurs in connection with previously proposed silver or silvergold alloy parts.
- Still another object is to provide an improved catalyst configuration for the purposes aforesaid which is structurally simple and relatively inexpensive to fabricate by use of standard shop processes.
- the invention contemplates deposition of a silver-gold alloy on nickel wire screen; the plated screen being then fabricated in the form of a stack of discs or cylindrical coils or other suitablecompactions of the plated screen material, preferably in the form of individual cups stacked in multiples thereof in the thrust chamber casing.
- FIG. l is a longitudinal sectional view through a thrust chamber equipped catalytic action, whereby maximum gas evolution and greatly improved response time is provided by means of a catalyst bed structure in accord with the present invention.
- the silver-gold alloy plating on the basis nickel wire screen components is provided in such manner that the silvergold alloy platings thereon are of nodular or other rugose surface form, as shown for example in FIG. 3.
- the catalyst component of the fabrication is of increased overall surface area-to-volume form; whereby an improved catalyst performance is obtained.
- the eiciency of the catalytic bed according to this invention is achieved in two-fold fashion. First, by the provision of a specific alloy and secondly, by the provision of specific surface characteristics of the catalytic material.
- any suitable means may be employed of course for plating the basis metal components of the catalyst bed with the silver-gold alloy surface coatings to obtain the fabrication illustrated and described hereinabove.
- the platings may be performed by a vapor deposition vmethod or by an electroplating method, as may be preferred.
- the electro-deposition plating method may be employed for example in accordance with the following procedure.
- Nickel wire mesh screen stock as obtained from any suitable commercial supplier thereof, is initially degreased by any suitable solvent such as tetrachlorethylene, and then further cleaned in an alkali bath, such as Oakite #24.
- the stock material is then water- Patented June 2, 1964 A rinsed and then activated in an acid nickel-chloride solution containing 32 ozs.
- nickel chloride per gallon and 11 fluid ozs. hydrochloric acid per gallon This solution is brought to a temperature 70 F., and a current density of 30 a.s.f. is applied; the' electrodes being of nickel metal.
- the tank is preferably rubber lined.
- the workpieces are connected to the anode terminal, for approximately 2 minutes, and then the current is reversed to make the workpieces cathodic for approximately 6 minutes; or in the alternative the workpieces may be soaked in the solution for about 15 minutes withoutfreversing the ,current flow. The workpieces are then again water-rinsed thoroughly.
- the workpieces are then placed in a silver-gold alloy plating tank wherein a platingsolution comprising potassium silver cyanide (double salt) 3 oz. per gallon; potassium gold cyanide (double salt) 0.024 o z. per gallon; potassium cyanide, 4 oz. per gallon; dipotassium sulphate, 4 oz. per gallon; and potassium carbonate, 2 oz. per gallon.
- This solution is worked at a temperature between 70-80 F., and under a voltage between 2-4 volts with a current density between 3-15 amperes per square foot.
- the tank kis preferably plastic or, rubber lined and the anodes are of stainless steel.
- the workpieces are immersed in the bath and initially from 4-6 amperes square vfoot are applied for approximately 11/2 hours. -This'provides a deposit layer of approximately .0015 inch thick.
- the workpieces are then cold water rinsed, and then hot water rinsed, and are then dried by blowing clean air or oven dried air thereover for approximately l/ hour at 212 F.-220 F.
- the deposit of silver-gold alloy on the nickel basis metal will be 1,'. found to comprise approximately 1.00% to 1.25% gold,
- the platings will be found to be of ⁇ substantially rugose surfaceV form, as shown for example in FIG. 3, whereby an improved catalyst surface-area versus,
- any other suitable physicalconguration of'silver-gold plated nickel basis metal may be employed, so long as the'latter is of sucient porosity to pass thel requisite ow of hydrogen peroxide gasto thc-thrust nozzle portion of the device.
- the present invention is equally applicable to any other catalyst bed requirement in connection with the decomposition of hydrogen peroxide.
- the catalyst bed of the invention may be employed' in conjunction with any form of gas generator, aswell as in a thrust chamber specifically, or wherever a catalyst is required to effect decomposition of hydrogen peroxide.
- a catalyst bed comprising a porous nickel metal mass the open surfaces of which are plated with ⁇ a silver-gold alloy comprising approximately 99% silver and 1% gold, the plating being deposited thereon in rugose surface form.
- An assembly for decomposition of hydrogen peroxide comprisingfa reaction chamber having an inlet for said hydrogen peroxide and an outlet for the products of decomposition, and a catalytic bed within said chamber comprising a porous mass located between saidy inletand said outlet and through which said hydrogen peroxide must pass, said mass-comprising a metallic base having thesurface areal thereof platedfwith an alloy consisting of gold and silver in which the silver is present in the amount of about 99%.
Description
June 2, 1964 MacDoNALD slLL THRUST CHAMBER CATALYST STRUCTURE Filed Q\ uvm. v\ #ru Hhml INVENTOR.
ATTORNEYS.
United States Patent O.F
3,135,703 THRUST CHAMBER CATALYST STRUCTURE MacDonald Sill, Buffalo, N.Y., assignor, by mesne assignments, to Bell Aerospace Corporation, Wheatiield, N.Y., a corporation of Delaware Filed Sept. 21, 1959, Ser. No. 841,173 3 Claims. (Cl. 252-474) This invention relates to improvements in monopropellent thrust chambers, and more particularly to an im proved catalyst bed device in a thrust chamber using 90% hydrogen peroxide as the propellent, for employment for example to provide attitude control effects in high altitude or space vehicles.
For some time it has been recognized that relatively small 90% hydrogen-peroxide thrust chambers may be effectively employed for space vehicle attitude control purposes, during high altitude or space flight where conventional -aerodynamic surfaces can no longer provide effective attitude control forces. The eiiiciency and relative simplicity of the 90% hydrogen peroxide thrust chamber for this purpose clearly indicates its desirability; and they have already been used with marked success for this purpose.
Among other critical features of the hydrogen-peroxide type rocket, the catalyst component is of particular importance; and various catalyst configurations have been previously used with a view to obtaining acceptable operation. For example, porous porcelain stones impregnated with calcium, potassium, or sodium permanganate have I been used. Also silver metal strips in various shapes and configurations have been employed; the silver sometimes being treated with samarium nitrate to increase its catalytic activity. Platinum has also been used as the catalyst metal; each catalyst metal and/or configuration having been previously designed to obtain maximum specific impulse and eiciency of the propellent use.
However, it is a primary object of the present invention to provide still further improvements in the art of catalyst bed constructions for use specifically in 90% hydrogen peroxide rocket chambers, gas generators, and the like.
A more specific object is to provide an improved catalyst bed as aforesaid which comprises a porous bed of catalyst metal parts having surface characteristics resulting in improved gas-evolution.
. Another object is to provide an improved catalyst bed as aforesaid providing greatly improved response time, due to an improved surface area-to-volume ratio.
Still another object is to provide an improved catalyst with one form of a catalyst bed construction of the present invention;
FIG. 2 is a sectional view through a detail of the catalyst bed component thereof; and
FIG. 3 is an enlarged scale schematic sectional view illustrating the form of the catalyst metal construction.
As shown in FIG.1, the invention is employed in conjunction with a rocket engine comprising generally a thrust chamber 10, which is of conventional form and includes a mounting flange portion 12; a catalyst bed chamber 14; and a thrust nozzle portion 16; it being understood that the present invention may be employed in conjunction with a thrust chamber of any other suitable design in lieu of the thrust chamber conguration shown in FIG. 1. However, as shown herein the hydrogen peroxide inlet port' is indicated at 18, and a dispersion plate vis provided as indicated at 20 to distribute the hydrogen peroxide uniformly throughout the cross section of the catalyst chamber 14. At the opposite end of the catalyst .chamber a perforate holding or blast dispersion plate 22 is provided to retain the catalyst bed in operative position while permitting the evolving gases to exit to the thrust nozzle 16.
As shown in FIG. 1, the thrust chamber 14 is arranged to be occupied by a stack of catalyst beds, each of which comprises a stainless steel cup designated 24 having an open bottom as indicated at 2'6 (FIG. 2) and supporting therein a series of wire meslr discs 28. As shown in FIG. 3 each disc 28 comprises a wire mesh fabrication of transversely woven nickel wire strands 30-30. It 'is a particular feature of the present invention that each wire mesh disc fabrication as shown herein comprises a basis metal fabrication of nickel wire strands 30 which are subsequently plated with silver-gold alloy layers as indicated at 32 (FIG. 3). It has been determined that a nickel Wire screen member, as a basis for the silver-gold valloy platings thereon, provides improved rigidity and heat resistant .characteristics for the overall structure, whereby the catalyst bed will be of improved overall resistance to fusing and/or attrition. At the same time,
the silver-gold alloy platings thereon provide optimum bed as aforesaid wherein the catalyst-surfaces are proas to provide improved rigidity of the bed, and improved resistance to fusing and attrition such as normally occurs in connection with previously proposed silver or silvergold alloy parts.
Still another object is to provide an improved catalyst configuration for the purposes aforesaid which is structurally simple and relatively inexpensive to fabricate by use of standard shop processes.
Other objects and advantages of the invention will appear in the specification hereinafter.
Generally stated, the invention contemplates deposition of a silver-gold alloy on nickel wire screen; the plated screen being then fabricated in the form of a stack of discs or cylindrical coils or other suitablecompactions of the plated screen material, preferably in the form of individual cups stacked in multiples thereof in the thrust chamber casing.
For example, as illustrated herein FIG. l is a longitudinal sectional view through a thrust chamber equipped catalytic action, whereby maximum gas evolution and greatly improved response time is provided by means of a catalyst bed structure in accord with the present invention.
It is another feature of the present invention that the silver-gold alloy plating on the basis nickel wire screen components is provided in such manner that the silvergold alloy platings thereon are of nodular or other rugose surface form, as shown for example in FIG. 3. By virtue of this arrangement the catalyst component of the fabrication is of increased overall surface area-to-volume form; whereby an improved catalyst performance is obtained.
Thus, the eiciency of the catalytic bed according to this invention is achieved in two-fold fashion. First, by the provision of a specific alloy and secondly, by the provision of specific surface characteristics of the catalytic material.
Any suitable means may be employed of course for plating the basis metal components of the catalyst bed with the silver-gold alloy surface coatings to obtain the fabrication illustrated and described hereinabove. For example, the platings may be performed by a vapor deposition vmethod or by an electroplating method, as may be preferred. The electro-deposition plating method may be employed for example in accordance with the following procedure. Nickel wire mesh screen stock, as obtained from any suitable commercial supplier thereof, is initially degreased by any suitable solvent such as tetrachlorethylene, and then further cleaned in an alkali bath, such as Oakite #24. The stock material is then water- Patented June 2, 1964 A rinsed and then activated in an acid nickel-chloride solution containing 32 ozs. nickel chloride per gallon and 11 fluid ozs. hydrochloric acid per gallon. This solution is brought to a temperature 70 F., and a current density of 30 a.s.f. is applied; the' electrodes being of nickel metal. The tank is preferably rubber lined. The workpieces are connected to the anode terminal, for approximately 2 minutes, and then the current is reversed to make the workpieces cathodic for approximately 6 minutes; or in the alternative the workpieces may be soaked in the solution for about 15 minutes withoutfreversing the ,current flow. The workpieces are then again water-rinsed thoroughly.
The workpieces are then placed in a silver-gold alloy plating tank wherein a platingsolution comprising potassium silver cyanide (double salt) 3 oz. per gallon; potassium gold cyanide (double salt) 0.024 o z. per gallon; potassium cyanide, 4 oz. per gallon; dipotassium sulphate, 4 oz. per gallon; and potassium carbonate, 2 oz. per gallon. This solution is worked at a temperature between 70-80 F., and under a voltage between 2-4 volts with a current density between 3-15 amperes per square foot. The tank kis preferably plastic or, rubber lined and the anodes are of stainless steel. First, with the current on, the workpieces are immersed in the bath and initially from 4-6 amperes square vfoot are applied for approximately 11/2 hours. -This'provides a deposit layer of approximately .0015 inch thick. The workpieces are then cold water rinsed, and then hot water rinsed, and are then dried by blowing clean air or oven dried air thereover for approximately l/ hour at 212 F.-220 F.
By virtue of the above described process, the deposit of silver-gold alloy on the nickel basis metal will be 1,'. found to comprise approximately 1.00% to 1.25% gold,
and the remainder silver. This specific alloy, on va nickel; basis metal structure, will provide optimum catalyst; performance for the purposes hereinaboveA described.-
' Furthermore, the platings will be found to be of `substantially rugose surfaceV form, as shown for example in FIG. 3, whereby an improved catalyst surface-area versus,
overall volume ratio will be provided.
It will of course be appreciated that in lieu of the specific stacked, wire mesh discforrn of catalyst bed as shown herein, any other suitable physicalconguration of'silver-gold plated nickel basis metal may be employed, so long as the'latter is of sucient porosity to pass thel requisite ow of hydrogen peroxide gasto thc-thrust nozzle portion of the device. Also, it is to be understood that the present invention is equally applicable to any other catalyst bed requirement in connection with the decomposition of hydrogen peroxide. For example, the catalyst bed of the invention may be employed' in conjunction with any form of gas generator, aswell as in a thrust chamber specifically, or wherever a catalyst is required to effect decomposition of hydrogen peroxide. Likewise, it will be understood that the outstanding feature ofthe present invention resides in the use of a b'asic metal'selected to, be of superior heat resistance and rigidity characteristics, such as are furnished by metals of the class of nickel, stainless steel alloys and the like; and that although only one form of the invention has been illustrated and described in detail hereinabove, it will be understood that various changes may be made therein without departing from the spirit of the invention or the scope of the following claims.
I claim:
1. In a thrust chamber of the type using hydrogen-peroxide monopropellent, a catalyst bed comprising a porous nickel metal mass the open surfaces of which are plated with` a silver-gold alloy comprising approximately 99% silver and 1% gold, the plating being deposited thereon in rugose surface form.
2. An assembly for decomposition of hydrogen peroxide, said assembly comprisingfa reaction chamber having an inlet for said hydrogen peroxide and an outlet for the products of decomposition, and a catalytic bed within said chamber comprising a porous mass located between saidy inletand said outlet and through which said hydrogen peroxide must pass, said mass-comprising a metallic base having thesurface areal thereof platedfwith an alloy consisting of gold and silver in which the silver is present in the amount of about 99%.
3.' The `.assembly ,according to claimA 2 in which said mass is rendered porous by electrodepositing said alloy on said base,'said base being nickel wire mesh.
References Cited in the le of this patent UNITED STATES PATENTS Re. 24,582 -Rinker Dec. 23, 1958 2,040,782 Van Peski May 12, 1936 2,791,883 Moore et al May 14,1957 -2,865,721 Lane et al Dec. 23, 1958 2,972,227 Allen Feb. 21, 1961 3,019,197 Saunders Jan. 30, 1962 3,056,663
Maglio et al. Oct. 2, 1962
Claims (1)
1. IN A THRUST CHAMBER OF THE TYPE USING 90% HYDROGEN-PEROXIDE MONOPROPELLENT, A CATALYST BED COMPRISING A POROUS NICKEL METAL MASS THE OPEN SURFACES OF WHICH ARE PLATED WITH A SILVER-GOLD ALLOY COMPRISING APPROXIMATELY
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US841173A US3135703A (en) | 1959-09-21 | 1959-09-21 | Thrust chamber catalyst structure |
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US841173A US3135703A (en) | 1959-09-21 | 1959-09-21 | Thrust chamber catalyst structure |
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Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3471106A (en) * | 1965-05-28 | 1969-10-07 | Rocket Research Corp | Valveless microrocket systems |
US3488962A (en) * | 1965-07-20 | 1970-01-13 | Fmc Corp | Method of decomposing hydrogen peroxide using a silver-palladium catalyst |
US3535879A (en) * | 1968-01-18 | 1970-10-27 | Aerojet General Co | Catalyst pack |
US3871828A (en) * | 1972-10-10 | 1975-03-18 | Hughes Aircraft Co | Hydrazine gas generator |
US3903693A (en) * | 1973-03-26 | 1975-09-09 | Anthony Fox | Rocket motor housing |
US3993600A (en) * | 1973-08-23 | 1976-11-23 | Matthey Bishop, Inc. | Catalyst support assembly |
US4027476A (en) * | 1973-10-15 | 1977-06-07 | Rocket Research Corporation | Composite catalyst bed and method for making the same |
US4047380A (en) * | 1976-04-09 | 1977-09-13 | The United States Of America As Represented By The Secretary Of The Navy | Combustion system using dilute hydrogen peroxide |
US4162292A (en) * | 1977-10-20 | 1979-07-24 | The United States Of America As Represented By The Secretary Of The Air Force | High pressure hydrazine gas generator |
US4698965A (en) * | 1981-04-17 | 1987-10-13 | Delchev Nedelko E | Hot gas source and fuel therefor |
US4795618A (en) * | 1984-09-26 | 1989-01-03 | Michael Laumen | Heat exchanger |
US4805399A (en) * | 1985-12-18 | 1989-02-21 | Rockcor Incorporated | Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust |
US4856271A (en) * | 1987-10-01 | 1989-08-15 | Olin Corporation | Gas generator and generating method employing dual catalytic and thermal liquid propellant decomposition paths |
US4967840A (en) * | 1990-01-18 | 1990-11-06 | Resource Production Management, Inc. | Process and apparatus for forming a gaseous stream for introduction into hydrocarbon bearing formations and gas generator therefor |
US6116014A (en) * | 1995-06-05 | 2000-09-12 | Catalytica, Inc. | Support structure for a catalyst in a combustion reaction chamber |
US20020110501A1 (en) * | 2000-11-13 | 2002-08-15 | John Barnes | Thermally tolerant support structure for a catalytic combustion catalyst |
WO2020154809A1 (en) * | 2019-01-30 | 2020-08-06 | Laboratoire Reaction Dynamics Inc. | Rocket engines |
US20220120240A1 (en) * | 2020-10-16 | 2022-04-21 | Sierra Nevada Corporation | Vortex thruster system including catalyst bed with screen assembly |
US11572851B2 (en) | 2019-06-21 | 2023-02-07 | Sierra Space Corporation | Reaction control vortex thruster system |
US11661907B2 (en) | 2018-10-11 | 2023-05-30 | Sierra Space Corporation | Vortex hybrid rocket motor |
US11879414B2 (en) | 2022-04-12 | 2024-01-23 | Sierra Space Corporation | Hybrid rocket oxidizer flow control system including regression rate sensors |
US11952965B2 (en) | 2019-01-30 | 2024-04-09 | Laboratoire Reaction Dynamics Inc. | Rocket engine's thrust chamber assembly |
US11952967B2 (en) | 2021-08-19 | 2024-04-09 | Sierra Space Corporation | Liquid propellant injector for vortex hybrid rocket motor |
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US2040782A (en) * | 1936-05-12 | Manufacture of olefine oxides | ||
US2791883A (en) * | 1951-10-25 | 1957-05-14 | Gen Electric | Propellant system |
USRE24582E (en) * | 1958-12-23 | Method and electrolyte for | ||
US2865721A (en) * | 1954-12-15 | 1958-12-23 | Napier & Son Ltd | Catalytic bed assemblies |
US2972227A (en) * | 1956-07-05 | 1961-02-21 | Bristol Siddeley Engines Ltd | Means for supplying a rocket motor with liquid fuel and concentrated hydrogen peroxide as propellant |
US3019197A (en) * | 1949-10-07 | 1962-01-30 | Charles E Saunders | Catalyst for the decomposition of hydrogen peroxide and method of preparing said catalyst |
US3056663A (en) * | 1959-06-15 | 1962-10-02 | Gen Electric | Catalyst decomposition chamber |
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US2040782A (en) * | 1936-05-12 | Manufacture of olefine oxides | ||
USRE24582E (en) * | 1958-12-23 | Method and electrolyte for | ||
US3019197A (en) * | 1949-10-07 | 1962-01-30 | Charles E Saunders | Catalyst for the decomposition of hydrogen peroxide and method of preparing said catalyst |
US2791883A (en) * | 1951-10-25 | 1957-05-14 | Gen Electric | Propellant system |
US2865721A (en) * | 1954-12-15 | 1958-12-23 | Napier & Son Ltd | Catalytic bed assemblies |
US2972227A (en) * | 1956-07-05 | 1961-02-21 | Bristol Siddeley Engines Ltd | Means for supplying a rocket motor with liquid fuel and concentrated hydrogen peroxide as propellant |
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Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3471106A (en) * | 1965-05-28 | 1969-10-07 | Rocket Research Corp | Valveless microrocket systems |
US3488962A (en) * | 1965-07-20 | 1970-01-13 | Fmc Corp | Method of decomposing hydrogen peroxide using a silver-palladium catalyst |
US3535879A (en) * | 1968-01-18 | 1970-10-27 | Aerojet General Co | Catalyst pack |
US3871828A (en) * | 1972-10-10 | 1975-03-18 | Hughes Aircraft Co | Hydrazine gas generator |
US3903693A (en) * | 1973-03-26 | 1975-09-09 | Anthony Fox | Rocket motor housing |
US3993600A (en) * | 1973-08-23 | 1976-11-23 | Matthey Bishop, Inc. | Catalyst support assembly |
US4027476A (en) * | 1973-10-15 | 1977-06-07 | Rocket Research Corporation | Composite catalyst bed and method for making the same |
US4047380A (en) * | 1976-04-09 | 1977-09-13 | The United States Of America As Represented By The Secretary Of The Navy | Combustion system using dilute hydrogen peroxide |
US4162292A (en) * | 1977-10-20 | 1979-07-24 | The United States Of America As Represented By The Secretary Of The Air Force | High pressure hydrazine gas generator |
US4698965A (en) * | 1981-04-17 | 1987-10-13 | Delchev Nedelko E | Hot gas source and fuel therefor |
US4795618A (en) * | 1984-09-26 | 1989-01-03 | Michael Laumen | Heat exchanger |
US4805399A (en) * | 1985-12-18 | 1989-02-21 | Rockcor Incorporated | Monopropellant plenum propulsion system with integrated valve/nozzle for fast response thrust |
US4856271A (en) * | 1987-10-01 | 1989-08-15 | Olin Corporation | Gas generator and generating method employing dual catalytic and thermal liquid propellant decomposition paths |
US4967840A (en) * | 1990-01-18 | 1990-11-06 | Resource Production Management, Inc. | Process and apparatus for forming a gaseous stream for introduction into hydrocarbon bearing formations and gas generator therefor |
US6116014A (en) * | 1995-06-05 | 2000-09-12 | Catalytica, Inc. | Support structure for a catalyst in a combustion reaction chamber |
US20020110501A1 (en) * | 2000-11-13 | 2002-08-15 | John Barnes | Thermally tolerant support structure for a catalytic combustion catalyst |
US7163666B2 (en) | 2000-11-13 | 2007-01-16 | Kawasaki Jukogyo Kabushiki Kaisha | Thermally tolerant support structure for a catalytic combustion catalyst |
US11661907B2 (en) | 2018-10-11 | 2023-05-30 | Sierra Space Corporation | Vortex hybrid rocket motor |
WO2020154809A1 (en) * | 2019-01-30 | 2020-08-06 | Laboratoire Reaction Dynamics Inc. | Rocket engines |
US11952965B2 (en) | 2019-01-30 | 2024-04-09 | Laboratoire Reaction Dynamics Inc. | Rocket engine's thrust chamber assembly |
US11572851B2 (en) | 2019-06-21 | 2023-02-07 | Sierra Space Corporation | Reaction control vortex thruster system |
US11927152B2 (en) | 2019-06-21 | 2024-03-12 | Sierra Space Corporation | Reaction control vortex thruster system |
US20220120240A1 (en) * | 2020-10-16 | 2022-04-21 | Sierra Nevada Corporation | Vortex thruster system including catalyst bed with screen assembly |
US11952967B2 (en) | 2021-08-19 | 2024-04-09 | Sierra Space Corporation | Liquid propellant injector for vortex hybrid rocket motor |
US11879414B2 (en) | 2022-04-12 | 2024-01-23 | Sierra Space Corporation | Hybrid rocket oxidizer flow control system including regression rate sensors |
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