CH480615A - Laminate material coating layer - Google Patents

Laminate material coating layer

Info

Publication number
CH480615A
CH480615A CH1558167A CH1558167A CH480615A CH 480615 A CH480615 A CH 480615A CH 1558167 A CH1558167 A CH 1558167A CH 1558167 A CH1558167 A CH 1558167A CH 480615 A CH480615 A CH 480615A
Authority
CH
Switzerland
Prior art keywords
coating layer
material coating
laminate material
laminate
layer
Prior art date
Application number
CH1558167A
Other languages
French (fr)
Original Assignee
Tech Du Verre Tisse S A R L
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 Tech Du Verre Tisse S A R L filed Critical Tech Du Verre Tisse S A R L
Publication of CH480615A publication Critical patent/CH480615A/en

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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52Protection, safety or emergency devices; Survival aids
    • B64G1/58Thermal protection, e.g. heat shields
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/42Streamlined projectiles
    • F42B10/46Streamlined nose cones; Windshields; Radomes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/34Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Medicine (AREA)
  • Remote Sensing (AREA)
  • General Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Health & Medical Sciences (AREA)
  • Thermal Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Woven Fabrics (AREA)
  • Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
CH1558167A 1966-11-08 1967-11-08 Laminate material coating layer CH480615A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR82923A FR1518681A (en) 1966-11-08 1966-11-08 Material for the constitution of so-called ablative structures protecting organs subjected to high temperatures

Publications (1)

Publication Number Publication Date
CH480615A true CH480615A (en) 1969-10-31

Family

ID=8620659

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1558167A CH480615A (en) 1966-11-08 1967-11-08 Laminate material coating layer

Country Status (6)

Country Link
US (1) US3583275A (en)
CH (1) CH480615A (en)
DE (1) DE1585546A1 (en)
FR (1) FR1518681A (en)
GB (1) GB1203440A (en)
SE (1) SE325781B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569237A1 (en) * 1984-08-14 1986-02-21 Aerospatiale THERMAL PROTECTION DEVICE RESISTANT TO ABLATION AND VIBRATION, AND METHOD OF MANUFACTURE
WO1991011676A2 (en) * 1990-01-26 1991-08-08 Colin Humphry Bruce Jack Hypervelocity drag reduction

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3949682A (en) * 1974-06-10 1976-04-13 The United States Of America As Represented By The Secretary Of The Navy Towline thermal protection system
US4519290A (en) * 1983-11-16 1985-05-28 Thiokol Corporation Braided preform for refractory articles and method of making
US4847063A (en) * 1987-12-02 1989-07-11 Fiber Materials, Inc. Hollow composite body having an axis of symmetry
FR2652036B1 (en) * 1989-09-19 1991-12-27 Aerospatiale THERMAL PROTECTIVE COATING, A PROCESS AND AN INSTALLATION FOR ITS MANUFACTURE.
US5232534A (en) * 1989-09-19 1993-08-03 Aerospatiale Soiete Nationale Industrielle Thermal protection coating, and method and installation for manufacturing it
GB2466793B (en) * 2009-01-07 2011-11-09 Ge Aviat Systems Ltd Composite spars
US8844877B1 (en) * 2010-09-02 2014-09-30 The Boeing Company Stay sharp, fail safe leading edge configuration for hypersonic and space access vehicles
DE102011113539B4 (en) * 2011-09-15 2015-10-01 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Thermal insulation for rocket engines
US8813626B2 (en) * 2012-11-19 2014-08-26 Chung Shan Institute Of Science And Technology, Armaments Bureau, M. N. D 3D braided composited tubes with throat sections and manufacture method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1367751A (en) * 1921-02-08 Howard i
CH6842A (en) * 1893-06-14 1893-10-31 Paul Walser & Cie Eyelet braid with rod threads
CH21450A (en) * 1901-05-21 1901-12-15 Fischer Gebr Fa Braid
US2467821A (en) * 1944-01-19 1949-04-19 Lynne D Gregg Sole and method of making the same
US2419829A (en) * 1944-05-13 1947-04-29 Internat Braid Company Woven fabric reinforcement
US3366001A (en) * 1964-12-11 1968-01-30 Johns Manville High strength-high temperature yarn

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569237A1 (en) * 1984-08-14 1986-02-21 Aerospatiale THERMAL PROTECTION DEVICE RESISTANT TO ABLATION AND VIBRATION, AND METHOD OF MANUFACTURE
EP0174886A1 (en) * 1984-08-14 1986-03-19 AEROSPATIALE Société Nationale Industrielle Thermal protecting device resistant to ablation and vibration, and production method therefor
US4655866A (en) * 1984-08-14 1987-04-07 Aerospatiale Societe Nationale Industrielle Device for thermal protection from ablation and vibrations and manufacturing method
WO1991011676A2 (en) * 1990-01-26 1991-08-08 Colin Humphry Bruce Jack Hypervelocity drag reduction
WO1991011676A3 (en) * 1990-01-26 1991-11-14 Colin Humphry Bruce Jack Hypervelocity drag reduction

Also Published As

Publication number Publication date
DE1585546A1 (en) 1970-09-17
SE325781B (en) 1970-07-06
US3583275A (en) 1971-06-08
GB1203440A (en) 1970-08-26
FR1518681A (en) 1968-03-29

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Legal Events

Date Code Title Description
PL Patent ceased