BE629028A - - Google Patents

Info

Publication number
BE629028A
BE629028A BE629028DA BE629028A BE 629028 A BE629028 A BE 629028A BE 629028D A BE629028D A BE 629028DA BE 629028 A BE629028 A BE 629028A
Authority
BE
Belgium
Prior art keywords
chamber
temperature
engine
coating
desc
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE629028A publication Critical patent/BE629028A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
BE629028D BE629028A (h)

Publications (1)

Publication Number Publication Date
BE629028A true BE629028A (h)

Family

ID=198672

Family Applications (1)

Application Number Title Priority Date Filing Date
BE629028D BE629028A (h)

Country Status (1)

Country Link
BE (1) BE629028A (h)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3459701A (en) * 1964-01-07 1969-08-05 Martin Marietta Corp Ceramic filled plastic system
US6904755B2 (en) 2000-01-21 2005-06-14 Alliant Techsystems, Inc. Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3459701A (en) * 1964-01-07 1969-08-05 Martin Marietta Corp Ceramic filled plastic system
US6904755B2 (en) 2000-01-21 2005-06-14 Alliant Techsystems, Inc. Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same

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