Ames Infusion Stories for NASA Annual Technology Report: Development of an Ablative 3D Quartz / Cyanate Ester Composite Multi-Functional Material for the Orion Spacecraft Compression PadVehicles re-entering Earth's atmosphere require protection from the heat of atmospheric friction. The Orion Multi-Purpose Crew Vehicle (MPCV) has more demanding thermal protection system (TPS) requirements than the Low Earth Orbit (LEO) missions, especially in regions where the structural load passes through. The use of 2-dimensional laminate materials along with a metal insert, used in EFT1 flight test for the compression pad region, are deemed adequate but cannot be extended for Lunar return missions.
Document ID
20160000687
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Smith, Brandon (NASA Ames Research Center Moffett Field, CA, United States)
Jan, Darrell Leslie (NASA Ames Research Center Moffett Field, CA, United States)
Venkatapathy, Ethiraj (NASA Ames Research Center Moffett Field, CA, United States)
IDRelationTitle20160000685See AlsoAmes Infusion Stories for NASA Annual Technology Report20160000686See AlsoAmes Infusion Stories for NASA Annual Technology Report: Nano Entry System for CubeSat-Class Payloads20160000685See AlsoAmes Infusion Stories for NASA Annual Technology Report