GB650444A - Improvements in or relating to a method of producing hot gases for the purpose of jet propulsion - Google Patents

Improvements in or relating to a method of producing hot gases for the purpose of jet propulsion

Info

Publication number
GB650444A
GB650444A GB14873/44A GB1487344A GB650444A GB 650444 A GB650444 A GB 650444A GB 14873/44 A GB14873/44 A GB 14873/44A GB 1487344 A GB1487344 A GB 1487344A GB 650444 A GB650444 A GB 650444A
Authority
GB
United Kingdom
Prior art keywords
liquid
fuels
hot gases
compounds containing
jet propulsion
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
Application number
GB14873/44A
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.)
Aerojet Rocketdyne Inc
Original Assignee
Aerojet Engineering Corp
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
Priority claimed from US486236A external-priority patent/US2573471A/en
Application filed by Aerojet Engineering Corp filed Critical Aerojet Engineering Corp
Publication of GB650444A publication Critical patent/GB650444A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/425—Propellants
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B27/00—Compositions containing a metal, boron, silicon, selenium or tellurium or mixtures, intercompounds or hydrides thereof, and hydrocarbons or halogenated hydrocarbons
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B39/00—Compositions containing free phosphorus or a binary compound of phosphorus, except with oxygen
    • 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
    • C06B47/04—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 a nitrogen oxide or acid thereof
    • 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
    • C06B47/08—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 hydrazine or a hydrazine derivative

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Abstract

A method of producing hot gases under pressure for the purpose of jet propulsion (see Groups XII and XXVI) comprises introducing a fuel comprising a liquid selected from the following list into a combustion chamber having an outlet orifice for hot gases and also introducing into the combustion chamber an oxidizing agent capable of reacting under atmospheric temperatures and pressures with the fuel to effect a spontaneous combustion thereof. The liquid fuels which may be used are (a) organic compounds containing at least one amide radicle such as aniline, orthotoluidine and methylamine; (b) liquid hydrocarbons containing large percentages of the amines mentioned in (a); (c) highly unsaturated hydrocarbons and compounds containing unsaturated hydrocarbon groups such as divinyl acetylene, dipropargyl and propargyl alcohol; (d) liquid hydrides of lithium, beryllium, boron, aluminium, magnesium, phosphorus, potassium and sodium; (e) liquid organo-metallic compounds containing one or more of the elements mentioned under (d); (f) liquid fuels containing one or more of the elements mentioned under (d) either in solution or in suspension; (g) the substances pyrrole, pyridine, pinene, terpin, pinol, terpineol and hydrazine; (h) ozonides; and (i) carbon disulphide containing dissolved phosphorus. These fuels may be used together with other fuels such as gasoline. Specification 592,706, [Group XXVI], is referred to.
GB14873/44A 1943-05-08 1944-08-03 Improvements in or relating to a method of producing hot gases for the purpose of jet propulsion Expired GB650444A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US486236A US2573471A (en) 1943-05-08 1943-05-08 Reaction motor operable by liquid propellants and method of operating it
US182742A US2693077A (en) 1943-05-08 1950-09-01 Reaction motor operable by liquid propellants and method of operating it

Publications (1)

Publication Number Publication Date
GB650444A true GB650444A (en) 1951-02-21

Family

ID=26878375

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14873/44A Expired GB650444A (en) 1943-05-08 1944-08-03 Improvements in or relating to a method of producing hot gases for the purpose of jet propulsion

Country Status (2)

Country Link
US (1) US2693077A (en)
GB (1) GB650444A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941005A (en) * 1955-07-29 1960-06-14 Phillips Petroleum Co 1, 2-diamino-1-alkene compounds
US3117415A (en) * 1959-04-02 1964-01-14 North American Aviation Inc Propellant and rocket propulsion method
US7083690B2 (en) 2001-07-03 2006-08-01 Wiley Organics, Inc. Catalyst system for rendering organic propellants hypergolic with hydrogen peroxide
WO2003104244A2 (en) * 2001-08-27 2003-12-18 Wiley Organics, Inc. Alkynylsilanes as fuels and rocket propellants
US8894782B2 (en) 2002-09-03 2014-11-25 Wiley Organics, Inc. Hypergolic hydrocarbon fuels

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE410616A (en) * 1932-07-29
US2573471A (en) * 1943-05-08 1951-10-30 Aerojet Engineering Corp Reaction motor operable by liquid propellants and method of operating it
GB576227A (en) * 1943-12-07 1946-03-25 George Frederick French Improvements in cycle stands

Also Published As

Publication number Publication date
US2693077A (en) 1954-11-02

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