GB582621A - Propellent explosives - Google Patents

Propellent explosives

Info

Publication number
GB582621A
GB582621A GB820442A GB820442A GB582621A GB 582621 A GB582621 A GB 582621A GB 820442 A GB820442 A GB 820442A GB 820442 A GB820442 A GB 820442A GB 582621 A GB582621 A GB 582621A
Authority
GB
United Kingdom
Prior art keywords
liquid
constituents
explosive
explosives
propellent
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
GB820442A
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.)
DONALD HUGH HALL
Original Assignee
DONALD HUGH HALL
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 DONALD HUGH HALL filed Critical DONALD HUGH HALL
Priority to GB820442A priority Critical patent/GB582621A/en
Publication of GB582621A publication Critical patent/GB582621A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/005Desensitisers, phlegmatisers

Abstract

582,621. Propellent explosives. HALL, D. H. June 15, 1942, Nos. 8204/42 and 11405/43. [Class 9 (ii)] A liquid or plastic propellent explosive, which can be fed to a combustion chamber at a greater rate than the rate of burning, comprises a relatively non-volatile liquid explosive such as nitroglycerine, and an organic solid or liquid diluent of low volatility miscible therewith. The proportions of the two constituents are preferably such that the calorific value ofthe resulting propellant lies between 700 and 1050 cal. /gm. Examples are given of suitable proportions by weight of the constituents to suit the liquid explosive used. The following examples of constituents are given.-For liquid explosives ethylene glycoldinitrate, diethylene glycoldinitrate, or nitroisobutyl glycerol trinitrate ; for liquid diluents : nitrobenzene, o-nitroanisole, or nitroparaffins; and for solid diluents: diethyl diphenyl urea, diphenylamine or dibutyl phthalate.
GB820442A 1942-06-15 1942-06-15 Propellent explosives Expired GB582621A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB820442A GB582621A (en) 1942-06-15 1942-06-15 Propellent explosives

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB820442A GB582621A (en) 1942-06-15 1942-06-15 Propellent explosives

Publications (1)

Publication Number Publication Date
GB582621A true GB582621A (en) 1946-11-22

Family

ID=9847854

Family Applications (1)

Application Number Title Priority Date Filing Date
GB820442A Expired GB582621A (en) 1942-06-15 1942-06-15 Propellent explosives

Country Status (1)

Country Link
GB (1) GB582621A (en)

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2971097A (en) * 1959-01-02 1961-02-07 Thompson Ramo Wooldridge Inc Control for a semi-solid monofuel driven turboalternator and pump system
US2988879A (en) * 1958-11-24 1961-06-20 Thompson Ramo Wooldridge Inc Rocket with fluid flame extinguisher for extruded fuel
US3003310A (en) * 1958-09-26 1961-10-10 Bar Dal Inc Combustion process employing irradiated solid polymeric fuels containing oxidizing agents
US3023573A (en) * 1959-03-23 1962-03-06 Atlantic Res Corp Rocket motor with fuel extrusion means
US3032979A (en) * 1959-01-02 1962-05-08 Thompson Ramo Wooldridge Inc Controlled feed rocket engine
US3041835A (en) * 1959-02-05 1962-07-03 Atlantic Res Corp Ignition aid
US3046736A (en) * 1958-02-10 1962-07-31 Thompson Ramo Wooldridge Inc Direction control for gelatin monopropellant rocket engine
US3067683A (en) * 1960-04-05 1962-12-11 Wolf Saul Means for regulating mass burning rate of solid propellants
US3067574A (en) * 1959-01-02 1962-12-11 Thompson Ramo Wooldridge Inc Thrust control for rocket engines
US3067575A (en) * 1959-01-02 1962-12-11 Thompson Ramo Wooldridge Inc Disposable rocket motor
US3070565A (en) * 1959-06-10 1962-12-25 Thompson Ramo Wooldridge Inc Apparatus for improved thrust cut-off
US3073120A (en) * 1959-02-05 1963-01-15 Atlantic Res Corp Igniter means for extruded plastic monopropellant
US3084504A (en) * 1959-05-26 1963-04-09 Thompson Ramo Wooldridge Inc Rocket engine
US3087306A (en) * 1959-02-05 1963-04-30 Atlantic Res Corp Extrusion device
US3088274A (en) * 1959-10-19 1963-05-07 Thompson Ramo Wooldridge Inc Dual thrust rocket engine
US3092968A (en) * 1957-11-06 1963-06-11 Atlantic Res Corp Process for generating gases and apparatus therefor
US3092959A (en) * 1957-11-06 1963-06-11 Atlantic Res Corp Process for generating gases and apparatus therefor
US3095334A (en) * 1957-11-06 1963-06-25 Atlantic Res Corp Thixotropic monopropellants
US3098625A (en) * 1960-12-19 1963-07-23 Thompson Ramo Wooldridge Inc Rocket motor and control system
US3105350A (en) * 1959-02-26 1963-10-01 Thompson Ramo Wooldridge Inc Monofuel propellant booster rocket
US3107187A (en) * 1959-02-05 1963-10-15 Atlantic Res Corp Propellant compositions
US3125853A (en) * 1964-03-24 mckinnon
US3126704A (en) * 1964-03-31 Process for generating gases and apparatus therefor
US3126701A (en) * 1964-03-31 Process for generating gases
US3128706A (en) * 1959-04-17 1964-04-14 Atlantic Res Corp Monopropellent grains
US3136669A (en) * 1958-10-17 1964-06-09 Spencer Chem Co Particulate polyolefin-liquid oxidizing agent propellant and rocket containing the same
US3154041A (en) * 1960-04-22 1964-10-27 Thompson Ramo Wooldridge Inc Monopropellant reaction motor having perforated wall propellant container
US3181982A (en) * 1959-04-29 1965-05-04 Phillips Petroleum Co Gel propellants comprising halogencontaining terpolymers
US3389026A (en) * 1959-12-08 1968-06-18 Navy Usa Plasticized high explosive and solid propellant compositions
US3533232A (en) * 1959-11-02 1970-10-13 Solid Fuels Corp Organic fusible solid fuel binders and stabilizers
GB2229176A (en) * 1983-03-04 1990-09-19 Rheinmetall Gmbh Liquid propellants
EP2128117A2 (en) * 2006-10-16 2009-12-02 Obshestvo S Ogranichennoy Otvetstvennjctyu "Ifokhim" Modifier for explosives

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126701A (en) * 1964-03-31 Process for generating gases
US3125853A (en) * 1964-03-24 mckinnon
US3126704A (en) * 1964-03-31 Process for generating gases and apparatus therefor
US3095334A (en) * 1957-11-06 1963-06-25 Atlantic Res Corp Thixotropic monopropellants
US3092968A (en) * 1957-11-06 1963-06-11 Atlantic Res Corp Process for generating gases and apparatus therefor
US3092959A (en) * 1957-11-06 1963-06-11 Atlantic Res Corp Process for generating gases and apparatus therefor
US3046736A (en) * 1958-02-10 1962-07-31 Thompson Ramo Wooldridge Inc Direction control for gelatin monopropellant rocket engine
US3003310A (en) * 1958-09-26 1961-10-10 Bar Dal Inc Combustion process employing irradiated solid polymeric fuels containing oxidizing agents
US3136669A (en) * 1958-10-17 1964-06-09 Spencer Chem Co Particulate polyolefin-liquid oxidizing agent propellant and rocket containing the same
US2988879A (en) * 1958-11-24 1961-06-20 Thompson Ramo Wooldridge Inc Rocket with fluid flame extinguisher for extruded fuel
US3067574A (en) * 1959-01-02 1962-12-11 Thompson Ramo Wooldridge Inc Thrust control for rocket engines
US3067575A (en) * 1959-01-02 1962-12-11 Thompson Ramo Wooldridge Inc Disposable rocket motor
US3032979A (en) * 1959-01-02 1962-05-08 Thompson Ramo Wooldridge Inc Controlled feed rocket engine
US2971097A (en) * 1959-01-02 1961-02-07 Thompson Ramo Wooldridge Inc Control for a semi-solid monofuel driven turboalternator and pump system
US3107187A (en) * 1959-02-05 1963-10-15 Atlantic Res Corp Propellant compositions
US3087306A (en) * 1959-02-05 1963-04-30 Atlantic Res Corp Extrusion device
US3073120A (en) * 1959-02-05 1963-01-15 Atlantic Res Corp Igniter means for extruded plastic monopropellant
US3041835A (en) * 1959-02-05 1962-07-03 Atlantic Res Corp Ignition aid
US3105350A (en) * 1959-02-26 1963-10-01 Thompson Ramo Wooldridge Inc Monofuel propellant booster rocket
US3023573A (en) * 1959-03-23 1962-03-06 Atlantic Res Corp Rocket motor with fuel extrusion means
US3128706A (en) * 1959-04-17 1964-04-14 Atlantic Res Corp Monopropellent grains
US3181982A (en) * 1959-04-29 1965-05-04 Phillips Petroleum Co Gel propellants comprising halogencontaining terpolymers
US3084504A (en) * 1959-05-26 1963-04-09 Thompson Ramo Wooldridge Inc Rocket engine
US3070565A (en) * 1959-06-10 1962-12-25 Thompson Ramo Wooldridge Inc Apparatus for improved thrust cut-off
US3088274A (en) * 1959-10-19 1963-05-07 Thompson Ramo Wooldridge Inc Dual thrust rocket engine
US3533232A (en) * 1959-11-02 1970-10-13 Solid Fuels Corp Organic fusible solid fuel binders and stabilizers
US3389026A (en) * 1959-12-08 1968-06-18 Navy Usa Plasticized high explosive and solid propellant compositions
US3067683A (en) * 1960-04-05 1962-12-11 Wolf Saul Means for regulating mass burning rate of solid propellants
US3154041A (en) * 1960-04-22 1964-10-27 Thompson Ramo Wooldridge Inc Monopropellant reaction motor having perforated wall propellant container
US3098625A (en) * 1960-12-19 1963-07-23 Thompson Ramo Wooldridge Inc Rocket motor and control system
GB2229176A (en) * 1983-03-04 1990-09-19 Rheinmetall Gmbh Liquid propellants
GB2229176B (en) * 1983-03-04 1991-01-09 Rheinmetall Gmbh Liquid propellants.
EP2128117A2 (en) * 2006-10-16 2009-12-02 Obshestvo S Ogranichennoy Otvetstvennjctyu "Ifokhim" Modifier for explosives
EP2128117A4 (en) * 2006-10-16 2013-10-30 Obshestvo S Ogranichennoy Otvetstvennjctyu Ifokhim Modifier for explosives

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