FR2366455A1 - Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon - Google Patents

Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon

Info

Publication number
FR2366455A1
FR2366455A1 FR7514239A FR7514239A FR2366455A1 FR 2366455 A1 FR2366455 A1 FR 2366455A1 FR 7514239 A FR7514239 A FR 7514239A FR 7514239 A FR7514239 A FR 7514239A FR 2366455 A1 FR2366455 A1 FR 2366455A1
Authority
FR
France
Prior art keywords
solid propellant
pref
elastomer
propylene
coating
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.)
Granted
Application number
FR7514239A
Other languages
French (fr)
Other versions
FR2366455B1 (en
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7514239A priority Critical patent/FR2366455A1/en
Publication of FR2366455A1 publication Critical patent/FR2366455A1/en
Application granted granted Critical
Publication of FR2366455B1 publication Critical patent/FR2366455B1/fr
Granted 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)

Abstract

An internal coating for a solid propellant rocket contains >=1 crosslinked elastomer, a loading material and an organosilicon. The elastomer is pref. partially crosslinked, and is an ethylene-propylene-terpolymer. The organosilicon is pref. a gamma-glycidoxypropyltrimethoxysilane. The coating pref. contains 1-10 pts. wt. silane per 100 pts. terpolymer, and also 1-2 pts. wt. 2,5-dimethyl 2,5-bis(t-butyl)hexane. A palsticizer can also be present and, the loading material is pref. a carbon black. The coating is used as a bond between the solid propellant and the metal body of the rocket, whether protected internally by a thermal rubber or not. It can be placed in position by glueing layers on the internal wall, thus allowing better control of thickness. It is of low density, and simple formula, and gives good adhesion to the solid propellant. The adhesion is durable, hence coated blocks of propellant can be stored.
FR7514239A 1975-04-29 1975-04-29 Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon Granted FR2366455A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7514239A FR2366455A1 (en) 1975-04-29 1975-04-29 Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7514239A FR2366455A1 (en) 1975-04-29 1975-04-29 Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon

Publications (2)

Publication Number Publication Date
FR2366455A1 true FR2366455A1 (en) 1978-04-28
FR2366455B1 FR2366455B1 (en) 1979-03-02

Family

ID=9154929

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7514239A Granted FR2366455A1 (en) 1975-04-29 1975-04-29 Internal coating for solid propellant rocket - contg. crosslinked ethylene!-propylene! elastomer and organo-silicon

Country Status (1)

Country Link
FR (1) FR2366455A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0116453A2 (en) * 1983-02-07 1984-08-22 Hercules Incorporated Process for lining composite rocket motor cases

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1567493A (en) * 1967-05-23 1969-05-16
US3686868A (en) * 1968-12-19 1972-08-29 Michael John Chase Rocket motors

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1567493A (en) * 1967-05-23 1969-05-16
US3686868A (en) * 1968-12-19 1972-08-29 Michael John Chase Rocket motors

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0116453A2 (en) * 1983-02-07 1984-08-22 Hercules Incorporated Process for lining composite rocket motor cases
EP0116453A3 (en) * 1983-02-07 1986-09-24 Hercules Incorporated Process for lining composite rocket motor cases

Also Published As

Publication number Publication date
FR2366455B1 (en) 1979-03-02

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