Various systems and methods of a layered tile insulation system of a space vehicle, configured to withstand vibration, high temperatures, and extreme thermal gradients, are disclosed. The layered tile insulation system can include at least one layered tile, each of the at least one layered tile including an outer layer having a first interlocking surface with a first set of interlocking features and an inner layer having a second interlocking surface with a second set of interlocking features, such that the outer layer is configured to be couple to the inner layer thereby forming a mechanical joint via the interlocking of the first interlocking surface with the second interlocking surface.
HIGH TEMPERATURE LAYERED TILE INSULATION SYSTEM FOR AEROSPACE VEHICLES
HOCHTEMPERATUR-SCHICHTFLIESENDÄMMUNG FÜR RAUMFAHRZEUGE
SYSTÈME D'ISOLATION DE CARREAUX EN COUCHES À HAUTE TEMPÉRATURE POUR VÉHICULES AÉROSPATIAUX
2022-10-26
Patent
Electronic Resource
English
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