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- Article name
- Structural inhomogeneities influence of carbon-carbon composite materials for hypersonic heat shield of aircraft on the spreads in ablating forms
- Authors
- BULYGIN M. G., , , State Rocket Centre "Makeyev Design Bureau", Chelyabinsk, Russia
KOSTIN G. F., , , State Rocket Centre "Makeyev Design Bureau", Chelyabinsk, Russia
TIKHONOV N. N., , , State Rocket Centre "Makeyev Design Bureau", Chelyabinsk, Russia
DEMENTYEV О. N., , , Chelyabinsk State University, Russia
KOVALEV Yu. М., , , Chelyabinsk State University, Russia
YAGAFAROV Sh. Sh., , , Chelyabinsk State University, Russia
- Keywords
- Year
- 2004 Issue 3 Pages 3 - 15
- Code EDN
- Code DOI
- Abstract
- Influence of the non-ablation of the different structural elements (threads, rods, matrix) of the carbon-carbon composite materials (CCCM), non-equal distribution of density and porosity in CCCM volume, mechanical ablation and impurities of particles ablated mechanically in boundary layer on the heat exchange and the material ablation rates spreads were investigated. Investigations carried out with use of the fire stand tests data and flight test results of special telemetry aircrafts with heat shield from CCCM.
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