GB1203440A - Improvements in or relating to sheathings or coverings for protecting parts exposed to verty high temperatures - Google Patents
Improvements in or relating to sheathings or coverings for protecting parts exposed to verty high temperaturesInfo
- Publication number
- GB1203440A GB1203440A GB50694/67A GB5069467A GB1203440A GB 1203440 A GB1203440 A GB 1203440A GB 50694/67 A GB50694/67 A GB 50694/67A GB 5069467 A GB5069467 A GB 5069467A GB 1203440 A GB1203440 A GB 1203440A
- Authority
- GB
- United Kingdom
- Prior art keywords
- verty
- sheathings
- coverings
- relating
- high temperatures
- 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
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
- F02K9/97—Rocket nozzles
- F02K9/974—Nozzle- linings; Ablative coatings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means 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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Health & Medical Sciences (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- Critical Care (AREA)
- Emergency Medicine (AREA)
- General Health & Medical Sciences (AREA)
- Remote Sensing (AREA)
- Fluid Mechanics (AREA)
- Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)
- Woven Fabrics (AREA)
Abstract
1,203,440. Spacecraft. TECHNIQUE DU VERRE TISSE. 8 Nov., 1967 [8 Nov., 1966], No. 50694/67. Heading B7W. [Also in Divisions B8, D1, F1 and F3] A heat shield for a spacecraft comprises a braid made of refractory yarns coated with plastics. The braid (see also Divisions D1-D2) is wound edge on to the surface to be protected and with its flat surfaces in face-to-face contact. The braiding yarns may be of silica, carbon fibres, metal or natural or man-made textile yarns.
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 |
---|---|
GB1203440A true GB1203440A (en) | 1970-08-26 |
Family
ID=8620659
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB50694/67A Expired GB1203440A (en) | 1966-11-08 | 1967-11-08 | Improvements in or relating to sheathings or coverings for protecting parts exposed to verty high temperatures |
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) |
Families Citing this family (11)
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 |
FR2569237B1 (en) * | 1984-08-14 | 1987-01-09 | Aerospatiale | ABLATION AND VIBRATION RESISTANT THERMAL PROTECTION DEVICE AND MANUFACTURING METHOD |
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 |
GB9001892D0 (en) * | 1990-01-26 | 1990-08-08 | Jack Colin | A technique for hypervelocity drag reduction by atmospheric heating |
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)
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 |
-
1966
- 1966-11-08 FR FR82923A patent/FR1518681A/en not_active Expired
-
1967
- 1967-11-07 DE DE19671585546 patent/DE1585546A1/en active Pending
- 1967-11-07 US US681188A patent/US3583275A/en not_active Expired - Lifetime
- 1967-11-07 SE SE15227/67A patent/SE325781B/xx unknown
- 1967-11-08 GB GB50694/67A patent/GB1203440A/en not_active Expired
- 1967-11-08 CH CH1558167A patent/CH480615A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
US3583275A (en) | 1971-06-08 |
DE1585546A1 (en) | 1970-09-17 |
SE325781B (en) | 1970-07-06 |
CH480615A (en) | 1969-10-31 |
FR1518681A (en) | 1968-03-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |