FIELD: chemistry.
SUBSTANCE: multilayer inner heat insulation of nose fairings consists of a temporary protective coating which is removed after assembling, aluminium- or steel-coated polyterephthalate or polyimide film, a heat insulation layer made from polymeric fibres, polyterephthalate or polyimide film, permanent adhesive layer and removable anti-adhesion paper (film), which is removed before gluing to the inner surface of the nose fairing.
EFFECT: faster assembling, reduced weight of heat insulation and reduced effect of heat on spacecraft.
2 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| SPACECRAFT THERMAL BLANKET WITH OUTER COMBINED LAYER | 2008 |
|
RU2397926C2 |
| THERMOSTATIC MATERIAL | 2012 |
|
RU2493058C1 |
| SPACECRAFT THERMAL BLANKET | 2013 |
|
RU2587740C2 |
| METHOD FOR ASSEMBLY OF INTERNAL HEAT AND SOUND INSULATION OF HEAD FAIRING OF CARRIER ROCKET | 2018 |
|
RU2707359C1 |
| ELECTROCONDUCTIVE ADHESIVE TAPE | 2009 |
|
RU2410298C1 |
| MATERIAL FOR SCREEN VACUUM THERMAL INSULATION AND METHOD OF ITS MANUFACTURE | 2017 |
|
RU2666884C1 |
| THERMOSTATIC MATERIAL | 2012 |
|
RU2493057C1 |
| FLEXIBLE MULTILAYER THIN-FILM RETROREFLECTIVE MATERIAL, METHOD OF OBTAINING RETROREFLECTIVE MATERIAL AND DEVICE FOR ITS OBTAINING | 2017 |
|
RU2660048C1 |
| INSULATION MATERIAL | 2020 |
|
RU2753045C1 |
| EROSIONPROOF, WEATHERPROOF, NONFLAMMABLE MULTILAYER MATERIAL | 2003 |
|
RU2235645C1 |
