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Technological principles of reducing the cycle time and improving the manufacturing safety of the thermal protection system for spacecraft reentry
| Authors: Tarasov V.A., Romanenkov V.A., Komkov M.A. | Published: 01.08.2014 |
| Published in issue: #8(653)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: reentry spacecraft, thermal protection system, woven filler, phenolformaldehyde binder, porous material impregnation time, modification of a binder by carbon nanotubes, complex autoclave |
