Strahlungsabschirmung mit einem Design zur Demise
Anmelder: Honeywell International Inc. 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4806792
- Anmeldetag
- 23. Februar 2026
- Veröffentlichung
- 16. September 2026
- Rechtsraum
- EP
- IPC
- B64G1/62
Abstract
A radiation shield is configured to destruct upon atmospheric reentry. The radiation shield includes first portions of a radiation shielding material (107-1) overlapping some or all of first surfaces of a substrate (102) of the radiation shield. The radiation shield includes second portions (107-2) of the radiation shielding material overlapping some or all of second surfaces of the substrate (102). As a result, radiation penetrating the radiation shield (through opposite surfaces of the radiation shield) is diminished due to coverage by such portions under such surfaces of the radiation shield. Further, because each of the first and the second portions are segmented, when the radiation shield, e.g., a payload at least partially enclosed by the radiation shield, re-enters atmosphere, the substrate will melt and/or evaporate permitting destruction of the radiation shield, e.g., and the payload protected thereby.
Anmelder
- Firma
- Honeywell International Inc.
- Land
- 🇺🇸 USA
US-amerikanischer Mischkonzern mit Schwerpunkten in Luft- und Raumfahrttechnik, Automatisierungslösungen, Gebäudetechnik sowie Spezialchemikalien und -materialien für Industrie- und Verteidigungskunden.
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