NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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)
Date Acquired
January 12, 2016
Publication Date
December 30, 2015
Subject Category
Man/System Technology And Life Support
Report/Patent Number
ARC-E-DAA-TN25366-3
Report Number: ARC-E-DAA-TN25366-3
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available