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Thermostructural Testing of PICA-D for NASA Planetary Science MissionsPhenolic Impregnated Carbon Ablator (PICA) has been flown as the heatshield TPS material for many NASA planetary science missions. Due to a supply issue with the heritage Rayon fibers used in PICA fabrication, NASA started a project in 2017 to develop a sustainable replacement for PICA using a domestic fiber source. Lyocell was identified as an alternative to the Rayon-based precursor leading to the development and testing of the replacement material, PICA-D (Domestic). PICA-D’s processing steps and manufacturing specification largely adopt those used for heritage PICA. Extensive material property and arcjet testing showed that PICA-D performance met the specification requirements, and its properties and thermal performance were largely in family with heritage PICA. PICA-D was selected as the heatshield TPS material for two upcoming NASA planetary science missions, the Dragonfly mission to Titan and Mars Sample Retrieval
Lander (SRL).
Document ID
20260001521
Acquisition Source
Ames Research Center
Document Type
Extended Abstract
Authors
Milad Mahzari
(Ames Research Center Mountain View, United States)
Keith Peterson
(Ames Research Center Mountain View, United States)
Derek Shannon
(Lockheed Martin Space System)
Matthew Gasch
(Ames Research Center Mountain View, United States)
Suman Muppidi
(Ames Research Center Mountain View, United States)
Michael Wright
(Ames Research Center Mountain View, United States)
Date Acquired
February 18, 2026
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 23rd International Planetary Probe Workshop
Location: Washington DC
Country: US
Start Date: June 20, 2026
End Date: June 26, 2026
Sponsors: National Aeronautics and Space Administration, Johns Hopkins University
Funding Number(s)
WBS: 258548.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Testing
Thermostructural
Titan
Mars
EDL
PICA-D
TPS
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