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Development of Advanced Lightweight Polymeric Foam Thermal Protection for Space Launch VehiclesLightweight thermal protective materials are essential for temperature regulation during ascent of space launch vehicles, especially for expendable launch vehicles and cryogenic propellant tanks. Among the lightest thermal protective materials commonly in use is polymeric foam, in the form of pour foam or spray-on foam insulation (SOFI). Foam processing is rapid, can accommodate large-scale or small-scale challenging geometries easily, and can be used in a climate controlled or non-climate-controlled setting. Application systems can be fixed or portable. Use-temperatures of foam range from cryogenic to those that will ablate the material.
Document ID
20240004669
Acquisition Source
Marshall Space Flight Center
Document Type
Poster
Authors
Elizabeth Schofield
(Jacobs (United States) Dallas, Texas, United States)
Angela Iler
(Marshall Space Flight Center Redstone Arsenal, United States)
John Bloyer
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
April 16, 2024
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: NASA In the Park
Location: Huntsville, AL
Country: US
Start Date: June 22, 2024
Sponsors: Marshall Space Flight Center, Downtown Huntsville, Inc.
Funding Number(s)
TASK: EM41.04.03.SSTG.TPS.01
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
TPS
Thermal Protection System
Sprayable Foam TPS
Foam Qualification
Launch Vehicle TPS
EM41 Capabilities
Foam Thermal Protection
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