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US3108432A - Method of rocket propulsion using organic polyperoxides - Google Patents

Method of rocket propulsion using organic polyperoxides Download PDF

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US3108432A
US3108432A US846239A US84623959A US3108432A US 3108432 A US3108432 A US 3108432A US 846239 A US846239 A US 846239A US 84623959 A US84623959 A US 84623959A US 3108432 A US3108432 A US 3108432A
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polyperoxide
polyperoxides
fuel
oxygen
same manner
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Balaceanu Jean-Claude
Clement Genevieve
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IFP Energies Nouvelles IFPEN
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    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/04—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
    • C06B45/06—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
    • C06B45/10—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin
    • C06B45/105—The resin being a polymer bearing energetic groups or containing a soluble organic explosive
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S149/00—Explosive and thermic compositions or charges
    • Y10S149/119—Oxidizer compounds

Definitions

  • This invention relates to improvements in fuels having high energy content and especially in rocket fuels, and more particularly to improvements in those combustible materials which are conventionally utilized in two-component chemical fuels.
  • rocket fuels are known as those combustible materials which require the higher energy content, the following description will refer more particularly to this kind of fuels. However, if will be understood that particulars of the present invention may as well be applied to any other kind of fuel requiring high energy content.
  • Rocket fuels are generally composed of twochemicals; one a material which yields an enormous quantity of energy upon being decomposed, and the second a very strong oxidizing agent.
  • the energy emitter are hydrocarbons, hydrazines, and boro-hydrides; and examples of strong oxidizing agents are nitric acid, hydrogen peroxide, perchlorates, liquid ozone and liquid oxygen, the most common oxidizing agent being liquid oxygen.
  • liquid oxygen contains no other carrier atoms, it is apparent that it constitutes a very concentrated oxidizing agent. It is easily recognized, however, that the utilization of liquid oxygen has many disadvantages due to the necessary low temperature liquefaction and concomitant storage problems in order to maintain the oxygen in the liquid state.
  • An object of the present invention is to improve rocket fuels by eliminating the disadvantages of the prior art fuels and by improving the performance of rockets.
  • Another object is to provide new fuel additives.
  • Still another object is to provide a method for producing polyperoxides.
  • the polyperoxides can be considered as copolymers of oxygen with a polymerizable compound such as an olet me or polyolefinic compound. They can be represented by the following general formula l fin in which R represents the polymerizable compound.
  • p'olyperoxides obtained from monoolefinic compounds the following may be used.
  • polyperoxides of the mono-olefins are for example: Polyperoxide of l,l-diphenylethylene Polyperoxide of a-methylstyrene Polyperoxide of indene Polyperoxide of ethylene Polyperoxide of propylene Polyperoxide of methylene Polyperoxide of isob-utylen'e Polyperoxides of pentenes Polyperoxide of 1,1-ditluorethylene Polyperoxide of vinylchloride
  • Other compounds such as the polyperoxides of the diolefins can actually be formed into several types of copolymers, the oxygen atoms being bonded to the carbon atoms in the 1,2 and/ or 1,4 positions. For example, the
  • polypenoxides of 2,3-dimethylbutadiene can be represented by the following two distinct formulae:
  • polyperoxides of butadiene and of isoprene can also be represented by a plurmity of configurations.
  • polyperoxide of cyclopentadiene Polyperoxide of 1,3-cyclohexadiene Polyperoxide of a-terpinene Polyperoxide of e-phellandrene Polyperoxide of fur-an Polyperoxide of alloocirnene Polyperoxide of chloroprene
  • the reaction is advantageously conducted in the liquid phase at tempera tures of about 0 to C. and preferably between 3550 C.
  • the latter is not critical for the formation of polyperoxides, as even outside of these temperature limits polyperoxides can be formed but comparatively inefiiciently.
  • the oxygen reactant is utilized in the gaseous form by itself or in mixture with an inert gas such as nitrogen.
  • an inert gas such as nitrogen.
  • One may operate under atmospheric pressure, although under higher pressures, the reaction rate is appreciably increased.
  • an initiator i.e. a compound which liberates free radicals at the temperature of the reaction.
  • Such chemical Compounds may be peroxides, for example, bcnzoyl peroxide, reactive azo compounds, for example, azo di-isobutyronit-rile, or analogs. It is obvious that one can also employ photochemical or radiochemical or other equivalent conventional reaction initiating techniques.
  • the obtained compounds can be isolated or concentrated by taldng advantage of their physical and physicochemical properties, but it is obviously necessary to avoid such conditions which would allow their possible decomposition.
  • these products may be dissolved in benzene or another aromatic solvent and re-precipitated by means of methanol, preferably below 0 C. It may also be of advantage to concentrate them by distillation or sublimation of their solvent in the cold under reduced pressure. Additional purification steps are generally unnecessary.
  • Example I An excess of gaseous oxygen is bubbled into styrene at temperatures "from about 50 C. in the presence of azodiisobutyronitrile at a concentration of about 0.02 mol per liter of styrene. After 24 'hours of oxygen absorption 20% of the theoretical amount of polyperoxide is obtained; the polyperoxide is precipitated by the addition of methanol at about 30 C., taken up in benzene and re-precipitated by means of methanol at the same temperature. It was then dried at 0 C. under reduced pressure (20 mm. Hg). The product thus obtained is a white solid, softening at about C. and melting at about l20l30 C.
  • Example II The same process as described above was successfully carried out utilizing benzoyl peroxide as an initiator.
  • Example 111 Example I was repeated successfully employing ultraviolet light as a photochemical initiator.
  • Example IV Example I was completed successfully employing the radiation of cobalt as a radiochemical initiator.
  • Example V In the same manner, described in Example I, a polyperoxide of acrylonitrile is formed.
  • Example VI In the same manner, described in Example I a poly peroxide of methyl methacrylate is formed.
  • Example VII In the same manner, described in Example I, peroxide of 1,1-diiluorethylene is formed.
  • Example VIII In the same manner, described in Example I, a polyperoxide of vinyl acetate is formed.
  • Example IX In the same manner, described in Example I, peroxide of 1.1-diphenylethylene is formed.
  • Example X a polyperoxide of wruethylstyrene is formed.
  • Example XI In the same manner, described in Example I, peroxide of indene is formed.
  • Example XII In the same manner, described in Example I, a polyperoxide of dimethylbutadiene is formed.
  • Example XIII In the same manner, described in Example I, peroxide of cyclopentadiene is formed.
  • Example XIV In the same manner, described in Example I,
  • Example XV In the same manner, described in Example I, a polyperoxide of a-terpinene is for-med.
  • Example XVI In the same manner, described in Example I, a polyperoxide of a-phellandrene is formed.
  • Example XVII In the same manner, described in Example I, peroxide of furan is formed.
  • Example XVIII In the same manner, described in Example I, peroxide of alloocirnene is formed.
  • Example XIX In the same manner, described in Example I, peroxide of vinyl chloride is formed.
  • Example XX a polya polya poly- Example XX
  • the products described in Examples I to XIX were mixed in the same manner as described in Example XX and were also found to yield unexpectedly good results.
  • Example XXII Example XX was repeated with a solution consisting of equal weights of the product produced in Example I and styrene. The energy release was substantially higher than with styrene alone.
  • the organic polyperoxides of this invention can be utilized either as fuels per se or as additives in conjunction with other conventional fuels or oxygen-containing solid or liquid oxidants, such as perchlorates, nitric acid, hydrogen peroxide, liquid ozone and liquid oxygen.
  • oxygen-containing solid or liquid oxidants such as perchlorates, nitric acid, hydrogen peroxide, liquid ozone and liquid oxygen.
  • the proportion of oxygen-containing material is chosen as to provide a substantially complete combustion of the fuel.
  • polyperoxides of this invention have also significant advantages as combustion-improving additives, even a very minor percentage added to a conventional fuel will be of great value.
  • a method for propelling rockets by means of the force developed by igniting therein a chemical composition consisting of a fuel and an oxidizing agent the improvement of adding thereto a minor amount of a polyeroxide selected from the group consisting of polyperoxides of styrene, acrylonitrile, methyl methacrylate, methaciylonitrile, vinyl acetate, 1,1-diflnoroethylene, vinylchloride, 1,1-diphenylethylene, a-methylstyrene, ethylene, propylene, isobutylene and pentenes.
  • a polyeroxide selected from the group consisting of polyperoxides of styrene, acrylonitrile, methyl methacrylate, methaciylonitrile, vinyl acetate, 1,1-diflnoroethylene, vinylchloride, 1,1-diphenylethylene, a-methylstyrene, ethylene, propylene, isobutylene and pen
  • a fuel composition consisting essentially of a major amount of a chemical composition consisting essentially of a fuel and an oxidizing agent and a minor amount of polyperoxide selected from the group consisting of poly peroxides of styrene, acrylonitrile, methyl methacry- 6 late, methacrylonitrile, vinyl acetate, 1,1-diiluoroethylene, vinylchloride, 1,1-diphenylethylene, a-rnethylstyrene, ethylene, propylene, isobutylene and pentenes.
  • a fuel composition according to claim 2 wherein the oxidizing agent is selected from the group consisting of solid and liquid oxidizing agents.
  • a fuel composition according to claim 2 wherein the oxidizing agent is hydrogen-peroxide.

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  • Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Molecular Biology (AREA)
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  • Organic Chemistry (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Description

United States Patent 3,l%3,432 METHGD F ROCKET KRQPULSKQN USING GRGANKC PGLYPERGXEES Jean-Claude Baiaceanu, Paris, and Genevieve Clement,
Coeuilly-Champigny, France, assignors to Kristitut Francais du letrole des llarhurants et Luhriiiants, Paris,
France No Drawing. Filed Get. 14, 1959, Ser. No. 846,239
Claims priority, application France Get. 16, 1 .953
8 Claims. (l. oil-35.4)
This invention relates to improvements in fuels having high energy content and especially in rocket fuels, and more particularly to improvements in those combustible materials which are conventionally utilized in two-component chemical fuels.
Since rocket fuels are known as those combustible materials which require the higher energy content, the following description will refer more particularly to this kind of fuels. However, if will be understood that particulars of the present invention may as well be applied to any other kind of fuel requiring high energy content.
. Rocket fuels are generally composed of twochemicals; one a material which yields an enormous quantity of energy upon being decomposed, and the second a very strong oxidizing agent. Examples of the energy emitter are hydrocarbons, hydrazines, and boro-hydrides; and examples of strong oxidizing agents are nitric acid, hydrogen peroxide, perchlorates, liquid ozone and liquid oxygen, the most common oxidizing agent being liquid oxygen.
In view of the fact that liquid oxygen contains no other carrier atoms, it is apparent that it constitutes a very concentrated oxidizing agent. It is easily recognized, however, that the utilization of liquid oxygen has many disadvantages due to the necessary low temperature liquefaction and concomitant storage problems in order to maintain the oxygen in the liquid state.
For many purposes the preparation and storage of liquid oxygen is so cumbersome that it is customary to utilize other strong oxidizing agents which do contain carrier atoms, such as perchlorates and hydrogen peroxide, which are normally either sol-id or liquid at pressures and temperatures of use. It is to be noted, however, that these latter compounds necessarily contain dead weight carrier atoms. This fact is important as the performance of rockets is closely connected to the ratio of Weight to energy release of fuel, the lower the Weight, other things being equal, the better the per-- formance. it can be seen, therefore, that conventional oxidizing agents in rocket fuels are either difficult to prepare, handle and store up, or they are comparatively in-eflicient because of dead weight.
An object of the present invention, therefore, is to improve rocket fuels by eliminating the disadvantages of the prior art fuels and by improving the performance of rockets.
Another object is to provide new fuel additives.
Still another object is to provide a method for producing polyperoxides.
Other objects and advantages of this invention will become apparent on further study of the specification and appended claims.
The objects of this invention are accomplished by utilizing a new concept in rocket fuels. Whereas prior art fuels contained a combustible material on the one hand, and an oxidizing material on the other hand, it has been discovered that great advantages can be obtained by utilizing a combustible material which also contains reactive forms of oxygen necessary for combustion. These compounds belong to the class of polyperoxides.
The polyperoxides can be considered as copolymers of oxygen with a polymerizable compound such as an olet me or polyolefinic compound. They can be represented by the following general formula l fin in which R represents the polymerizable compound.
As examples of p'olyperoxides obtained from monoolefinic compounds, the following may be used. Polyperoxide of styrene:
(-OCHOHzO-)n C5115 Polyperoxide of acrylonitrile:
(OCHa?HO-) Polyperoxide of methyl methacrylate:
C O O CH:
(OCH2-(1-O) a Polyperoxide of methacrylonitrile:
.(lJN (-O-OH:?-O)Q Polyperoxide of vinyl acetate:
(OCH2CHO) 11 Other polyperoxides of the mono-olefins are for example: Polyperoxide of l,l-diphenylethylene Polyperoxide of a-methylstyrene Polyperoxide of indene Polyperoxide of ethylene Polyperoxide of propylene Polyperoxide of methylene Polyperoxide of isob-utylen'e Polyperoxides of pentenes Polyperoxide of 1,1-ditluorethylene Polyperoxide of vinylchloride Other compounds such as the polyperoxides of the diolefins can actually be formed into several types of copolymers, the oxygen atoms being bonded to the carbon atoms in the 1,2 and/ or 1,4 positions. For example, the
polypenoxides of 2,3-dimethylbutadiene can be represented by the following two distinct formulae:
Likewise the polyperoxides of butadiene and of isoprene can also be represented by a plurmity of configurations.
Polyperoxide of cyclopentadiene Polyperoxide of 1,3-cyclohexadiene Polyperoxide of a-terpinene Polyperoxide of e-phellandrene Polyperoxide of fur-an Polyperoxide of alloocirnene Polyperoxide of chloroprene These polyperoxides can be obtained by the reaction of oxygen on olefins and polyolefins. The reaction is advantageously conducted in the liquid phase at tempera tures of about 0 to C. and preferably between 3550 C. Although the best results are obtained in that temperature range, the latter is not critical for the formation of polyperoxides, as even outside of these temperature limits polyperoxides can be formed but comparatively inefiiciently. For example, it is necessary to avoid very low temperatures which would result in very low reaction rates or very high temperatures at which the compounds would decompose. The oxygen reactant is utilized in the gaseous form by itself or in mixture with an inert gas such as nitrogen. One may operate under atmospheric pressure, although under higher pressures, the reaction rate is appreciably increased.
In order to initiate the reaction or increase its rate, it is generally preferred to employ an initiator, i.e. a compound which liberates free radicals at the temperature of the reaction. Such chemical Compounds may be peroxides, for example, bcnzoyl peroxide, reactive azo compounds, for example, azo di-isobutyronit-rile, or analogs. It is obvious that one can also employ photochemical or radiochemical or other equivalent conventional reaction initiating techniques.
The obtained compounds can be isolated or concentrated by taldng advantage of their physical and physicochemical properties, but it is obviously necessary to avoid such conditions which would allow their possible decomposition. Thus it is often possible to isolate them by adding to their solutions at a temperature preferably below C., for example at about C., such solids or liquids which reduce their solubility, for example methanol. If desired, these products may be dissolved in benzene or another aromatic solvent and re-precipitated by means of methanol, preferably below 0 C. It may also be of advantage to concentrate them by distillation or sublimation of their solvent in the cold under reduced pressure. Additional purification steps are generally unnecessary.
The above described procedures can be carried out either continuously, or by a batch process.
In order to explain this invention better, attention is directed to the following examples which however are not intended to be lirnitative of the appended claims.
Example I An excess of gaseous oxygen is bubbled into styrene at temperatures "from about 50 C. in the presence of azodiisobutyronitrile at a concentration of about 0.02 mol per liter of styrene. After 24 'hours of oxygen absorption 20% of the theoretical amount of polyperoxide is obtained; the polyperoxide is precipitated by the addition of methanol at about 30 C., taken up in benzene and re-precipitated by means of methanol at the same temperature. It Was then dried at 0 C. under reduced pressure (20 mm. Hg). The product thus obtained is a white solid, softening at about C. and melting at about l20l30 C.
Example II The same process as described above was successfully carried out utilizing benzoyl peroxide as an initiator.
Example 111 Example I was repeated successfully employing ultraviolet light as a photochemical initiator.
Example IV Example I was completed successfully employing the radiation of cobalt as a radiochemical initiator.
Example V In the same manner, described in Example I, a polyperoxide of acrylonitrile is formed.
Example VI In the same manner, described in Example I a poly peroxide of methyl methacrylate is formed.
i Example VII In the same manner, described in Example I, peroxide of 1,1-diiluorethylene is formed.
Example VIII In the same manner, described in Example I, a polyperoxide of vinyl acetate is formed.
Example IX In the same manner, described in Example I, peroxide of 1.1-diphenylethylene is formed.
a polya poly- Example X In the same manner, described in Example I, a polyperoxide of wruethylstyrene is formed.
Example XI In the same manner, described in Example I, peroxide of indene is formed.
Example XII In the same manner, described in Example I, a polyperoxide of dimethylbutadiene is formed.
Example XIII In the same manner, described in Example I, peroxide of cyclopentadiene is formed.
Example XIV In the same manner, described in Example I,
a polya polya polyperoxide of 1.3-cycl0hexadiene is formed.
Example XV In the same manner, described in Example I, a polyperoxide of a-terpinene is for-med.
Example XVI In the same manner, described in Example I, a polyperoxide of a-phellandrene is formed.
Example XVII In the same manner, described in Example I, peroxide of furan is formed.
Example XVIII In the same manner, described in Example I, peroxide of alloocirnene is formed.
Example XIX In the same manner, described in Example I, peroxide of vinyl chloride is formed.
a polya polya poly- Example XX The products described in Examples I to XIX were mixed in the same manner as described in Example XX and were also found to yield unexpectedly good results.
Example XXII Example XX was repeated with a solution consisting of equal weights of the product produced in Example I and styrene. The energy release was substantially higher than with styrene alone.
In general, the organic polyperoxides of this invention can be utilized either as fuels per se or as additives in conjunction with other conventional fuels or oxygen-containing solid or liquid oxidants, such as perchlorates, nitric acid, hydrogen peroxide, liquid ozone and liquid oxygen. Preferably, the proportion of oxygen-containing material is chosen as to provide a substantially complete combustion of the fuel.
Since the polyperoxides of this invention have also significant advantages as combustion-improving additives, even a very minor percentage added to a conventional fuel will be of great value.
It is considered that even a small percentage of polyperoxide within the fuel will be of some value as even a small percentage of oxygen reduces the necessary amount of other strong oxidizing compounds and facilitates the combustion. Of course, the higher the percentage of oxygen within the molecule, the more efficient will be the fuel and thus the performance of the rocket, per fuel weight unit.
Of course, these fuels are useful for propelling all types of vehicles which utilize rocket-type fuel.
it will be understood that this invention is susceritible to other modifications in order to adapt it to the different usages and conditions, such as in the process of manufacturing a polyperoxide of styrene any unreacted styrene can be recovered by vacuum distillation and used over again, and accordingly it is desired to comprehend such modifications within the invention as may fall within the scope of the appended claims.
What is claimed is:
1. In a method for propelling rockets by means of the force developed by igniting therein a chemical composition consisting of a fuel and an oxidizing agent, the improvement of adding thereto a minor amount of a polyeroxide selected from the group consisting of polyperoxides of styrene, acrylonitrile, methyl methacrylate, methaciylonitrile, vinyl acetate, 1,1-diflnoroethylene, vinylchloride, 1,1-diphenylethylene, a-methylstyrene, ethylene, propylene, isobutylene and pentenes.
2. A fuel composition consisting essentially of a major amount of a chemical composition consisting essentially of a fuel and an oxidizing agent and a minor amount of polyperoxide selected from the group consisting of poly peroxides of styrene, acrylonitrile, methyl methacry- 6 late, methacrylonitrile, vinyl acetate, 1,1-diiluoroethylene, vinylchloride, 1,1-diphenylethylene, a-rnethylstyrene, ethylene, propylene, isobutylene and pentenes.
3. A fuel composition according to claim 2 wherein the oxidizing agent is selected from the group consisting of solid and liquid oxidizing agents.
4. A fuel composition according to claim 2 wherein the oxidizing agent is a perchlorate.
5. A fuel composition according to claim 2 wherein the oxidizing agent is nitric-acid.
6. A fuel composition according to claim 2 wherein the oxidizing agent is hydrogen-peroxide.
7. A fuel composition according to claim 2 wherein the oxidizing agent is ozone.
8. A fuel composition according to claim 2 wherein the oxidizing agent is liquid oxygen.
References (Iited in the file of this patent UNITED STATES PATENTS 2,563,305 Britten et al. Aug. 7, 1951 2,729,936 Britton Jan. 10, 1956 2,767,208 Miller et a1. Oct. 16, 1956 2,794,055 Russell et a1 May 28, 1957 2,795,618 Emerson et al June 11, 1957 2,879,276 Mayo Mar. 24, 1959 2,896,401 Zletz July 28, 1959 2,898,377 Handy et a1 Aug. 4, 1959 2,899,469 lones Aug. 11, 1959 2,911,436 Miller et a1. Nov. 3, 1959 2,971,949 Anderson et a1 Feb. 14, 1961 OTHER REFERENCES Zaellringer: Solid Propeilant Rockets Second Stage American Rocket (10., Box 1112 Wyandotte, Mich, 1958,
pp. 207-212 and 229.

Claims (1)

1. IN A METHOD FOR PROPELLING ROCKETS BY MEANS OF THE FORCE DEVELOPED BY IGNITING THEREIN A CHEMICAL COMPOSITION CONSISTING OF A FUEL AND AN OXIDIZING AGENT, THE IMPROVEMENT OF ADDING THERETO A MINOR AMOUNT OF A POLYPEROXIDE SELECTED FROM THE GROUP CONSISTING OF POLYPEROXIDES OF STYRENE, ACRYLONITRILE, METHYL METHACRYLATE, METHACRYLONITRILE, VINYL ACETAE, 1,1-DIFLUOROETHYLENE, VINYLCHLORIDE, 1,1-DIPHENYLETHYLENE, A-METHYLSTYENE, ETHYLENE, PROPYLENE, ISOBUTYLENE AND PENTENES.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3235422A (en) * 1963-03-22 1966-02-15 United Aircraft Corp Fluorocarbon propellant
US3976602A (en) * 1964-12-31 1976-08-24 Shell Oil Company Highly unsaturated polyethers
US4653380A (en) * 1984-06-15 1987-03-31 Fmc Corporation Bipropellant gun and method of firing same
US20160152739A1 (en) * 2013-06-18 2016-06-02 Evonik Degussa Gmbh Isocyanate/siloxane polyether composition

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563305A (en) * 1948-07-29 1951-08-07 Phillips Petroleum Co Coating of pulse-jet valve elements
US2729936A (en) * 1950-04-24 1956-01-10 Phillips Petroleum Co Fuel for and method of operating a jet engine
US2767208A (en) * 1953-09-08 1956-10-16 Gen Electric Method of making carbonyl compounds by decomposing polymeric vinyl peroxides
US2794055A (en) * 1957-05-28 Catalytic hydrogenation of styrene
US2795618A (en) * 1953-06-26 1957-06-11 Monsanto Chemicals Organic peroxides
US2879276A (en) * 1956-05-31 1959-03-24 Gen Electric Oxide formation
US2896401A (en) * 1953-02-16 1959-07-28 Standard Oil Co Rocket propulsion method
US2898377A (en) * 1953-02-27 1959-08-04 Du Pont Polymeric butadiene peroxide
US2899469A (en) * 1959-08-11 Hydroperoxides of tertiary alkyl
US2911436A (en) * 1953-09-08 1959-11-03 Gen Electric Method of preparing polymeric peroxides
US2971949A (en) * 1958-08-14 1961-02-14 Du Pont Fluorinated polymeric peroxides

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2794055A (en) * 1957-05-28 Catalytic hydrogenation of styrene
US2899469A (en) * 1959-08-11 Hydroperoxides of tertiary alkyl
US2563305A (en) * 1948-07-29 1951-08-07 Phillips Petroleum Co Coating of pulse-jet valve elements
US2729936A (en) * 1950-04-24 1956-01-10 Phillips Petroleum Co Fuel for and method of operating a jet engine
US2896401A (en) * 1953-02-16 1959-07-28 Standard Oil Co Rocket propulsion method
US2898377A (en) * 1953-02-27 1959-08-04 Du Pont Polymeric butadiene peroxide
US2795618A (en) * 1953-06-26 1957-06-11 Monsanto Chemicals Organic peroxides
US2767208A (en) * 1953-09-08 1956-10-16 Gen Electric Method of making carbonyl compounds by decomposing polymeric vinyl peroxides
US2911436A (en) * 1953-09-08 1959-11-03 Gen Electric Method of preparing polymeric peroxides
US2879276A (en) * 1956-05-31 1959-03-24 Gen Electric Oxide formation
US2971949A (en) * 1958-08-14 1961-02-14 Du Pont Fluorinated polymeric peroxides

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3235422A (en) * 1963-03-22 1966-02-15 United Aircraft Corp Fluorocarbon propellant
US3976602A (en) * 1964-12-31 1976-08-24 Shell Oil Company Highly unsaturated polyethers
US4653380A (en) * 1984-06-15 1987-03-31 Fmc Corporation Bipropellant gun and method of firing same
US20160152739A1 (en) * 2013-06-18 2016-06-02 Evonik Degussa Gmbh Isocyanate/siloxane polyether composition

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