ES8603163A1 - Procedimiento para preparar un material propulsor solido para cohetes, basado en un aglutinante hidrocarbonado y una sal inorganica de plomo. - Google Patents

Procedimiento para preparar un material propulsor solido para cohetes, basado en un aglutinante hidrocarbonado y una sal inorganica de plomo.

Info

Publication number
ES8603163A1
ES8603163A1 ES535857A ES535857A ES8603163A1 ES 8603163 A1 ES8603163 A1 ES 8603163A1 ES 535857 A ES535857 A ES 535857A ES 535857 A ES535857 A ES 535857A ES 8603163 A1 ES8603163 A1 ES 8603163A1
Authority
ES
Spain
Prior art keywords
lead
propellant
oxidizing material
binder
oxidizing
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
ES535857A
Other languages
English (en)
Other versions
ES535857A0 (es
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.)
Universal Propulsion Co Inc
Original Assignee
Universal Propulsion Co Inc
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 US06/530,956 external-priority patent/US4619722A/en
Application filed by Universal Propulsion Co Inc filed Critical Universal Propulsion Co Inc
Publication of ES8603163A1 publication Critical patent/ES8603163A1/es
Publication of ES535857A0 publication Critical patent/ES535857A0/es
Granted 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
    • C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
    • C06B33/12—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide the material being two or more oxygen-yielding compounds

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Liquid Carbonaceous Fuels (AREA)

Abstract

PROCEDIMIENTO PARA PREPARAR UN MATERIAL PROPULSOR SOLIDO PARA COHETES, BASADO EN UN AGLUTINANTE HIDROCARBONADO Y UNA SAL INORGANICA DE PLOMO. CONSISTE EN INCLUIR COMO SAL DE PLOMO AL NITRATO, PEROXIDO O YODATO ENTRE EL 83% Y 91% EN PESO Y CARBONO HASTA EL 10% EN PESO COMO AGLUTINANTE. ES POSIBLE LA UTILIZACION DE UN OXIDANTE ADICIONAL COMO EL CLORATO POTASICO.
ES535857A 1983-09-12 1984-09-12 Procedimiento para preparar un material propulsor solido para cohetes, basado en un aglutinante hidrocarbonado y una sal inorganica de plomo. Granted ES535857A0 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/530,956 US4619722A (en) 1983-09-12 1983-09-12 Propellant material with oxidizer reduction to lead oxide
US54785483A 1983-11-02 1983-11-02

Publications (2)

Publication Number Publication Date
ES8603163A1 true ES8603163A1 (es) 1985-12-16
ES535857A0 ES535857A0 (es) 1985-12-16

Family

ID=27063417

Family Applications (1)

Application Number Title Priority Date Filing Date
ES535857A Granted ES535857A0 (es) 1983-09-12 1984-09-12 Procedimiento para preparar un material propulsor solido para cohetes, basado en un aglutinante hidrocarbonado y una sal inorganica de plomo.

Country Status (5)

Country Link
EP (1) EP0141163B1 (es)
BR (1) BR8404538A (es)
DE (2) DE141163T1 (es)
ES (1) ES535857A0 (es)
IL (1) IL72838A (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2291478B (en) * 1990-03-26 1996-07-10 Marconi Co Ltd Lithium-water reactor

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1571251A1 (de) * 1966-08-24 1971-09-30 Bundesrep Deutschland Nicht-hygroskopischer und perchloratfreier bzw.perchloratarmer Composite-Double-Base-Festtreibstoff
US3834956A (en) * 1967-08-08 1974-09-10 Hercules Inc Solid propellant composition containing lead and lead compounds
US3945202A (en) * 1970-08-27 1976-03-23 Universal Propulsion Co. Rocket containing lead oxidizer salt-high density propellant

Also Published As

Publication number Publication date
BR8404538A (pt) 1985-08-06
EP0141163A1 (en) 1985-05-15
DE141163T1 (de) 1986-04-30
DE3475398D1 (en) 1989-01-05
EP0141163B1 (en) 1988-11-30
ES535857A0 (es) 1985-12-16
IL72838A (en) 1989-01-31

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