Castable thermal insulation for use as heat shields
Source abstract
Abstract
Structural members supporting the afterburners of high thrust rocket engines are subjected to extreme heating, along with severe vibration and high acceleration levels during early lift-off. Chemically-bonded, castable, zircon composite foams were developed and successfully tested to meet specific, laboratory simulated lift-off conditions.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Rocket and propulsion systems research · Gas Dynamics and Kinetic Theory · Energetic Materials and Combustion
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References
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