US3345821A - Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use - Google Patents

Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use Download PDF

Info

Publication number
US3345821A
US3345821A US135402A US13540261A US3345821A US 3345821 A US3345821 A US 3345821A US 135402 A US135402 A US 135402A US 13540261 A US13540261 A US 13540261A US 3345821 A US3345821 A US 3345821A
Authority
US
United States
Prior art keywords
liquid
difluoramino
tetranitromethane
mole
fuel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US135402A
Inventor
Ellington M Magee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ExxonMobil Technology and Engineering Co
Original Assignee
Exxon Research and Engineering Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Exxon Research and Engineering Co filed Critical Exxon Research and Engineering Co
Priority to US135402A priority Critical patent/US3345821A/en
Application granted granted Critical
Publication of US3345821A publication Critical patent/US3345821A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B43/00—Compositions characterised by explosive or thermic constituents not provided for in groups C06B25/00 - C06B41/00
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
    • C06B47/02—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant
    • C06B47/10—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant a component containing free boron, an organic borane or a binary compound of boron, except with oxygen
    • 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
    • C06D5/08—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of two or more liquids

Definitions

  • a stable liquid propellant combination of high performance is found to be provided by using a liquid difluoramino substituted and saturated compound such as those containing 1 NF group per carbon and containing at least 1 NE, group per 2 H atoms, with liquid tetranitromethane.
  • a liquid difluoramino substituted and saturated compound such as those containing 1 NF group per carbon and containing at least 1 NE, group per 2 H atoms, with liquid tetranitromethane.
  • the liquid difluoramino saturated compounds include bis(difluoramino) ethane C H -(NF tris (difluoramino) propane C H (NF tetrakis (NF tetrahydrofuran tetrakis (difluoramino) butane C H (NF pentakis (difluoramino) pentane C H (NF C H (NF and C H (NF as particularly useful ingredients.
  • the useful liquid difluoramino alkanes for the present purposes contain 2 to 7 carbon atoms per molecule with an NF group attached to each carbon atom.
  • Mixtures of these compounds may be used satisfactorily together in combination with the oxygen supplying oxidizer tetranitromethane, C(NO).
  • the resulting liquid mixture may be made to be used as a monopropellant system which supplies both fuel and oxidizing constitutents (fluorine and oxygen).
  • liquid propellant it may be introduced into the combustion zone of a rocket where a suitable igniter, e.g. squib, spark or glow plug or a hypergolic material, initiates ignition.
  • a suitable igniter e.g. squib, spark or glow plug or a hypergolic material
  • the liquid mixtuer of the difluoramino alkane and tetranitromethane is useful in a bipropell-ant system which admixes a liquid borohydride, e.g. -B H B H and B H with these oxidizers in the combustion zone.
  • a liquid borohydride e.g. -B H B H and B H with these oxidizers in the combustion zone.
  • the container walls for storage in or out of the rocket casing can be thinner, thus increasing the propellant load capacity.
  • the hardware for flowing and metering can thus be simplified, also.
  • the C(NO plus liquid difluoramino alkane mixture can be used in a bipropellant system with liquid borohydrides to obtain a still higher specific impulse.
  • the molar ratios of the mixed liquid oxidizers and of the borohydride fuel can be changed without substantial changes in the resulting impulse; however, for highest impulses the ratios are balanced to form as principal exhaust products, BOF, CO, HF, H
  • liquid fuels For example liquefied diborane B H may be used and also liquid alkyl decaboranes. If desired, small proportions of compatible thickening agents and powdered flammable metals e.g. boron, aluminum or the like may be dispersed in the liquid fuel.
  • the mixed, liquid oxidizers, C(NO and difluoramino alkanes may be thickened with stable and compatible difluoramino polymers having close to 1 NF per carbon without detracting drastically from their high performance.
  • the amount of thickening is kept low to prevent sticking and to avoid undesired retardation of flow.
  • the stable C(NO +liquid difluoramino alkane mixtures are of exceptional value in attaining very high thrust performance used by themselves or with particularly good liquid fuels, e.g. the borohydrides, they have still other exceptional values. They may be used to oxidize lower energy fuels, if desired. They are particularly interesting in being capable of high Isp values particularly with relatively low exhaust gas temperatures, which is of concern in preventing burning-out of exhaust nozzles.
  • from about 0.2 to 1.4 mole of C(NO is mixed with 1 mole of the difiuoramino compound represented as having the composition C I-I (NF n being 2 to 7, and depending upon the proportion of the hydrocarbon group (C H present.
  • the optimum mole ratio of the C(NO to the difiuoramino alkane C H (NF is close to n/ 7in/ 20, wherein n is 2 to 7.
  • the C(NO h-l-difiuoramino compound liquid mixtures can have a varied ratio of oxygen to carbon over a range without substantial loss in performance and with the advantage of relatively low exhaust gas temperatures when the O/ C ratio is low. This holds even when the difluoramino-hydrocarbon components do not have quite 1 NF group per carbon.
  • the compounds having CNF groups have the average composition C H (NF and these compounds are mixed for combustion with liquid C(NO the optimum ratio for maximum specific impulse is close to 1.25 mole C(NO per mole of the C H (NF liquid but this ratio can be lowered to 1 without much loss in performance yet with a drop of about 300 C. in the exhaust gas temperature.
  • the ratio of (NF to hydrogen is 1:2, of F/H is 1:1 and of NF /C is 4:5.
  • the difluoramino compounds of the C H (NF type perform like C H (NF in having 1 F/ 1H atom ratio.
  • Another compound of this type is tetrakis (N1 cyclohexane, C H (NF)
  • these difluoramino compounds are termed para-alkanes.
  • the para-alkanes thus include the difluoramino-alkanes difluoramino-cycloalkancs, and difiuoramino-epoxyalkanes (e.g. tetrakis (N1 tetrahydrofuran as tetrakis (N1 1,4-epoxy butane).
  • difluoramino-alkanes difluoramino-cycloalkancs
  • difiuoramino-epoxyalkanes e.g. tetrakis (N1 tetrahydrofuran as tetrakis (N1 1,4-epoxy butane).
  • a stable oxidizer and fuel liquid mixture consisting essentially of tetranitromethane in a 0.2 to 1.4 mole proportion and a 1 mole proportion of a compatible liquid C to C difluoramino para-alkane containing at least 1 NF group for each two hydrogen atoms in the paraalkane molecule.
  • composition as defined in claim 1 in which the para-alkane contains 1 NF group per carbon atom.
  • a stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid bis (N1 ethane.
  • a stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid tris (N1 propane.
  • a stable oxidizer and fuel liquid mixture consisting essentially of a 0,2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid tetrakis (NF butane.
  • a stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid pentakis (N1 cyclohexane.
  • a method of developing thrust by combustion of oi-propellant oxidizer and fuel components in a combustion chamber which comprises injecting into the combustion chamber a liquid stream of liquid C(NO mixed in a 0.2 to 1.4 mole proportion with a 1 mole proportion of liquid C to C para-alkane containing at least 1 NF group per 2 hydrogen atoms in the molecule and simultaneously injecting into the combustion chamber a stream of liquid borohydride as fuel.
  • a method of developing thrust by combustion of a liquid mono-propellant which comprises injecting into a combustion chamber a liquid stream consisting essentially of liquid C(NO mixed in a 0.2 to 1 mole proportion with a 1 mole proportion of liquid difluoramino C to C para-alkane containing 1 NF group per two hydrogen atoms.
  • the monopropellant is a liquid mixture of C(NO and bis (NF ethane.

Description

United States Patent Oflfice 3,345,821 STORABLE LIQUID RUCKET PROPELLANTS CONTAINING TETRANITROMETHANE WITH DIFLTETORAMKNO COMPOUNDS AND METHGD F U E Ellington M. Magee, Scotch Plains, N.J., assignor to {Esso Research and Engineering Company, a corporation of Delaware No Drawing. Filed Aug. 21, 1961, Ser. No. 135,402 12 Claims. (Cl. 60214) 1 This invention relates to high-performance liquid propellant compositions for use in rockets. It is concerned more particularly with a formulation of such liquid oxidizer compositions which are stable liquids under ordinary conditions and storable.
Known, high performance liquid propellants, including a liquid oxidizer, have the disadvantage of being nonstorable, e.g., systems such as H +F N H and N H +O These systems involve the use of a liquefied normally gaseous oxidizer.
Now in accordance with the present invention a stable liquid propellant combination of high performance is found to be provided by using a liquid difluoramino substituted and saturated compound such as those containing 1 NF group per carbon and containing at least 1 NE, group per 2 H atoms, with liquid tetranitromethane. These ingredients, which provide both fuel and oxidizer constitutents can be mixed and safely stored.
The liquid difluoramino saturated compounds include bis(difluoramino) ethane C H -(NF tris (difluoramino) propane C H (NF tetrakis (NF tetrahydrofuran tetrakis (difluoramino) butane C H (NF pentakis (difluoramino) pentane C H (NF C H (NF and C H (NF as particularly useful ingredients. In general, the useful liquid difluoramino alkanes for the present purposes contain 2 to 7 carbon atoms per molecule with an NF group attached to each carbon atom. Mixtures of these compounds may be used satisfactorily together in combination with the oxygen supplying oxidizer tetranitromethane, C(NO The resulting liquid mixture may be made to be used as a monopropellant system which supplies both fuel and oxidizing constitutents (fluorine and oxygen).
To use the liquid propellant, it may be introduced into the combustion zone of a rocket where a suitable igniter, e.g. squib, spark or glow plug or a hypergolic material, initiates ignition.
The liquid mixtuer of the difluoramino alkane and tetranitromethane is useful in a bipropell-ant system which admixes a liquid borohydride, e.g. -B H B H and B H with these oxidizers in the combustion zone.
The following examples illustrate propellant formulations of the present invention.
EXAMPLE 1 Using a liquid mixture of 0.2857 mole C(NO per mole of bis(difluoramino) ethane, the density of the mixture is about 1.53. The determined specific impulse (Isp) of this mixture in pounds thrust per pounds flow of the mixture per second is 305 seconds. The performance factor of this mixture is about 466, this factor being directly proportional to the product of the density and specific impulse. This performance factor is of most importance in evaluating the relative merits of various liquid propellants. Thus, the performance factor of 466 for the mixture of C H (NF plus C(NO is higher 7 than that of other high performance liquid propellant compositions except N H plus liquid oxygen, which is not a storable combination.
3,345,821 Patented Oct. 10, 1967 The liquid mixture of C(NO and his (NF ethane is a unique monopropellant in which oxidizing and fuel constituents are satisfactorily balanced even if the ratios of these compounds are varied. Although both these components have been thought of as oxidizers, no other fuel need be admixed.
In using the normally liquid propellant ingredients, e.g. C(NO and the liquid difluoramino alkanes, the container walls for storage in or out of the rocket casing can be thinner, thus increasing the propellant load capacity. The hardware for flowing and metering can thus be simplified, also.
The C(NO plus liquid difluoramino alkane mixture can be used in a bipropellant system with liquid borohydrides to obtain a still higher specific impulse.
EXAMPLE 2 TAB LE System Isp D (Density) D Isp C (N O2)-l+O2H4 (NF2)2 305 1. 53 466 H Fz 372 0. 82 305 N sH4F2 362 1. 32 4'78 NzHiN204 290 1. 23 357 Of the systems liste din the table, the only system other than C(NO +C H (NF which is liquid at ordinary atmospheric temperatures is N H N O.,. It is evident that the C(NO +C H (NF system is much better than the latter in performance. Moreover, N H -N O components do not make a stable storable mixture.
EXAMPLE 3 Mixing a molar ratio of 1.287 moles C(NO L, per mole of tris (NF propane, this liquid oxidizer mixture can be stored indefinitely and can be supplied to a combustion chamber to burn B H supplied thereto as liquid at a rate of 2.83 moles per mole of the tris (NF propane in the C(NO mixture to give an impulse of 326 seconds.
The molar ratios of the mixed liquid oxidizers and of the borohydride fuel can be changed without substantial changes in the resulting impulse; however, for highest impulses the ratios are balanced to form as principal exhaust products, BOF, CO, HF, H
Other variations may be made in selection of liquid fuels. For example liquefied diborane B H may be used and also liquid alkyl decaboranes. If desired, small proportions of compatible thickening agents and powdered flammable metals e.g. boron, aluminum or the like may be dispersed in the liquid fuel.
The mixed, liquid oxidizers, C(NO and difluoramino alkanes, may be thickened with stable and compatible difluoramino polymers having close to 1 NF per carbon without detracting drastically from their high performance. The amount of thickening is kept low to prevent sticking and to avoid undesired retardation of flow.
It is believed that by using the liquid mixture of oxygen oxidizer, C(NO and a liquid difluoramino alkane as fluorine oxidizer the highest specific impulse and performance is obtained in comparison to any other system using a stable oxidizer and fuel mixture.
While the stable C(NO +liquid difluoramino alkane mixtures are of exceptional value in attaining very high thrust performance used by themselves or with particularly good liquid fuels, e.g. the borohydrides, they have still other exceptional values. They may be used to oxidize lower energy fuels, if desired. They are particularly interesting in being capable of high Isp values particularly with relatively low exhaust gas temperatures, which is of concern in preventing burning-out of exhaust nozzles. For this purpose, from about 0.2 to 1.4 mole of C(NO is mixed with 1 mole of the difiuoramino compound represented as having the composition C I-I (NF n being 2 to 7, and depending upon the proportion of the hydrocarbon group (C H present. Thus, preferably the optimum mole ratio of the C(NO to the difiuoramino alkane C H (NF is close to n/ 7in/ 20, wherein n is 2 to 7.
The C(NO h-l-difiuoramino compound liquid mixtures can have a varied ratio of oxygen to carbon over a range without substantial loss in performance and with the advantage of relatively low exhaust gas temperatures when the O/ C ratio is low. This holds even when the difluoramino-hydrocarbon components do not have quite 1 NF group per carbon. For example, in a system where the compounds having CNF groups have the average composition C H (NF and these compounds are mixed for combustion with liquid C(NO the optimum ratio for maximum specific impulse is close to 1.25 mole C(NO per mole of the C H (NF liquid but this ratio can be lowered to 1 without much loss in performance yet with a drop of about 300 C. in the exhaust gas temperature. In this particular system the ratio of (NF to hydrogen is 1:2, of F/H is 1:1 and of NF /C is 4:5.
The difluoramino compounds of the C H (NF type perform like C H (NF in having 1 F/ 1H atom ratio. Another compound of this type is tetrakis (N1 cyclohexane, C H (NF Accordingly, in a broad sense the present invention discloses that the liquid oxygen oxidizer is mixed with a compatible (mutually stable in the mixture) liquid difluoramino compound, which contains 2 to 7 carbon atoms per molecule, is saturated (contains no C=C bonds), and contains at least 1 NF group per 2 H atoms. For brevity, these difluoramino compounds are termed para-alkanes. The para-alkanes thus include the difluoramino-alkanes difluoramino-cycloalkancs, and difiuoramino-epoxyalkanes (e.g. tetrakis (N1 tetrahydrofuran as tetrakis (N1 1,4-epoxy butane).
Modifications and variations falling within the scope of this invention are defined in the claims.
What is claimed is:
1. A stable oxidizer and fuel liquid mixture consisting essentially of tetranitromethane in a 0.2 to 1.4 mole proportion and a 1 mole proportion of a compatible liquid C to C difluoramino para-alkane containing at least 1 NF group for each two hydrogen atoms in the paraalkane molecule.
2. A composition as defined in claim 1 in which the para-alkane is an alkane.
3. A composition as defined in claim 1, in which the para-alkane is a cycloalkane.
4. A composition as defined in claim 1 in which the para-alkane is an epoxy alkane.
5. A composition as defined in claim 1 in which the para-alkane contains 1 NF group per carbon atom.
6. A stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid bis (N1 ethane.
7. A stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid tris (N1 propane.
8. A stable oxidizer and fuel liquid mixture consisting essentially of a 0,2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid tetrakis (NF butane.
9. A stable oxidizer and fuel liquid mixture consisting essentially of a 0.2 to 1.4 mole proportion of liquid C(NO and a 1 mole proportion of liquid pentakis (N1 cyclohexane.
10. A method of developing thrust by combustion of oi-propellant oxidizer and fuel components in a combustion chamber which comprises injecting into the combustion chamber a liquid stream of liquid C(NO mixed in a 0.2 to 1.4 mole proportion with a 1 mole proportion of liquid C to C para-alkane containing at least 1 NF group per 2 hydrogen atoms in the molecule and simultaneously injecting into the combustion chamber a stream of liquid borohydride as fuel.
11. A method of developing thrust by combustion of a liquid mono-propellant which comprises injecting into a combustion chamber a liquid stream consisting essentially of liquid C(NO mixed in a 0.2 to 1 mole proportion with a 1 mole proportion of liquid difluoramino C to C para-alkane containing 1 NF group per two hydrogen atoms.
12. The method defined in claim 11, in Which the monopropellant is a liquid mixture of C(NO and bis (NF ethane.
No references cited.
BENJAMIN R. PADGETT, Primary Examiner.
LEON D. ROSDOL, OSCAR R. VERTIZ, Examiners.

Claims (1)

10. A METHOD OF DEVELOPING THRUST BY COMBUSTION OF BI-PROPELLANT OXIDIZER AND FUEL COMPONENTS IN A COMBUSTION CHAMBER WHICH COMPRISES INJECTING INTO THE COMBUSTION CHAMBER A LIQUID STREAM OF LIQUID C(NO2)4 MIXED IN A 0.2 TO 1.4 MOLE PROPORTION WITH A 1 MOLE PROPORTION OF LIQUID C2 TO C7 PARA-ALKANE CONTAINING AT LEAST 1 NF2 GROUP PER 2 HYDROGEN ATOMS IN THE MOLECULE AND SIMULTANEOUSLY INJECTING INOT THE COMBUSTION CHAMBER A STREAM OF LIQUID BOROHYDRIDE AS FUEL.
US135402A 1961-08-21 1961-08-21 Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use Expired - Lifetime US3345821A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US135402A US3345821A (en) 1961-08-21 1961-08-21 Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US135402A US3345821A (en) 1961-08-21 1961-08-21 Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use

Publications (1)

Publication Number Publication Date
US3345821A true US3345821A (en) 1967-10-10

Family

ID=22467953

Family Applications (1)

Application Number Title Priority Date Filing Date
US135402A Expired - Lifetime US3345821A (en) 1961-08-21 1961-08-21 Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use

Country Status (1)

Country Link
US (1) US3345821A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3383859A (en) * 1962-09-10 1968-05-21 Army Usa Dinitrogen tetraoxide-difluoroaminosubstituted fuel compositions and method of usingsame for rocket propulsion
US3447323A (en) * 1967-07-26 1969-06-03 Us Army Hypergolic method for igniting high energy difluoroamino compounds
US3534554A (en) * 1963-06-25 1970-10-20 Us Army High energy liquid fluoroaminomethane storable high energy oxidizer and method of propulsion
US4938814A (en) * 1988-07-08 1990-07-03 European Space Agency High-performance propellant combinations for a rocket engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3383859A (en) * 1962-09-10 1968-05-21 Army Usa Dinitrogen tetraoxide-difluoroaminosubstituted fuel compositions and method of usingsame for rocket propulsion
US3534554A (en) * 1963-06-25 1970-10-20 Us Army High energy liquid fluoroaminomethane storable high energy oxidizer and method of propulsion
US3447323A (en) * 1967-07-26 1969-06-03 Us Army Hypergolic method for igniting high energy difluoroamino compounds
US4938814A (en) * 1988-07-08 1990-07-03 European Space Agency High-performance propellant combinations for a rocket engine
US4950341A (en) * 1988-07-08 1990-08-21 European Space Agency High-performance propellant combinations for a rocket engine

Similar Documents

Publication Publication Date Title
US4938814A (en) High-performance propellant combinations for a rocket engine
Lempert et al. Energetic performances of solid composite propellants
US3083527A (en) Hybrid rocket propulsion process
US3088272A (en) Stable propellants
US3171249A (en) Propellant and rocket propulsion method employing hydrazine with amino tetrazoles
US3345821A (en) Storable liquid rocket propellants containing tetranitromethane with difluoramino compounds and method of use
US4316359A (en) Method of imparting hypergolicity to non-hypergolic rocket propellants
US2951335A (en) Stable propellants
US5837930A (en) Propellants, in particular for the propulsion of vehicles such as rockets, and process for their preparation
US3257802A (en) Method of hybrid high specific impulse propulsion using lithium-polyethylene solid with chlorine containing oxidizers
US3921394A (en) Heterogeneous monopropellant compositions and thrust producing method
US3925124A (en) Heterogeneous monopropellant compositions
US3196059A (en) Thixotropic propellant compositions
US3213609A (en) High energy propellant and process employing hydrazines and nitro compounds
US3170281A (en) Method of producing thrust by hydrogenation of an acetylenic hydrocarbon
US3613371A (en) Hypergolic bipropellant propulsion process using boron components
US2944385A (en) Stable monopropellants
US2769304A (en) Hypergolic fuel and the method of using it
US2930684A (en) Propellant combination including liquid fluorine and liquid oxide oxidizer
US2771738A (en) Morpholines as hypergolic fuels
US3043099A (en) Monopropellant fuel
US3230700A (en) Rocket propulsion method using hydrocarbon fuels containing aminoalkyl acrylate polymers
US3705495A (en) Fuel systems and oxidizers
US3095693A (en) Oxidizer comprising tetranitromethane and nitrogen pentoxide and method of producingthrust therewith
US3696616A (en) Non-carbon forming monopropellant process using a lower alkylhydrazine and ammonia