FIELD: aeronautical engineering.
SUBSTANCE: proposed wing has skin with transversal and longitudinal primary structure. Vehicle is also provided with thermal protection made on base of quartz plates with external radiation coat; they are mounted on skin through compensating substrate. Wing is provided with coat made from capillary porous material which is applied to inner surfaces of compartments formed by skin and primary structure. Vehicle is provided with steam-discharge pipe unions communicating the compartments with upper surface of wing.
EFFECT: improved thermal protection.
2 dwg
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APPARATUS FOR HEAT PROTECTION OF AN AIRCRAFT | 2021 |
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RU2763917C1 |
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VAPORIZER | 2020 |
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REUSABLE AEROSPACE CREFT | 0 |
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ANTENNA DOME | 2017 |
|
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AIRCRAFT THERMAL PROTECTION DEVICE | 2017 |
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RU2657614C1 |
ANTENNA FAIRING | 2018 |
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RU2748531C1 |
ANTENNA DOME | 2013 |
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RU2536339C1 |
Authors
Dates
2007-05-27—Published
1985-01-02—Filed