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Qualification of Domestic Lyocell Based Phenolic Impregnated Carbon Ablator (PICA-D) for NASA MissionsPhenolic Impregnated Carbon Ablator (PICA) is a low-density ablator that has been used as the planetary entry heatshield for several NASA missions since the late 90’s. Its low density and efficient performance characteristics have proven effective for use from Discovery to Flag-ship class missions, from Sample Return missions such as Stardust, OSIRIS-REx to large Mars Lander missions such as Mars Science Lab (MSL) and Mars 2020. The rayon-based carbon precursor raw material used in PICA preform manufacturing has experienced multiple supply chain issues. The challenge involved in finding a replacement fiber source is in processing as well as in the final performance of the ablator. Each replacement necessitates the requalification of the PICA. This has happened at least twice in the past 25 years, and a third substitution is now needed.

Due to the obsolescence of the input foreign rayon fiber source, a new variant of PICA has been developed using a domestic rayon-like fiber source, Lyocell. Due to its flight heritage and proven capability, PICA is baselined as the Thermal Protection System (TPS) for Dragonfly and Mars Sample Return Sample Retrieval Lander mission and is being considered for the backshell of the Mars Sample Return Earth Entry System. All three missions are due to be launched between 2026 and 2028. The challenge this time is to ensure the PICA made with domestic material is a suitable replacement to the heritage PICA used in MSL and Mars 2020 so that the design of the heatshield can be matured without much risk. Results are presented from the recent efforts of 22 PICA-D billets that were Lot Acceptance Tested. Thermal, mechanical, and representative environment arc-jet tests have been conducted. Testing of PICA-Domestic (PICA-D) indicates very comparable performance with respect to “heritage” PICA materials and thus PICA-D is expected to be a sustainable and nearly a “drop-in” replacement solution for future NASA missions.
Document ID
20220006119
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Matt Gasch
(Ames Research Center Mountain View, California, United States)
Mairead Stackpoole
(Ames Research Center Mountain View, California, United States)
Ethiraj Venkatapathy
(Ames Research Center Mountain View, California, United States)
Don Ellerby
(Ames Research Center Mountain View, California, United States)
Frank Milos
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Keith Peterson
(Ames Research Center Mountain View, California, United States)
Kristina Skokova
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Jonathan Morgan
(Ames Research Center Mountain View, California, United States)
Dinesh Prabhu
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Jeremie Meurisse
(Science and Technology Corp. Moffett Field, CA, United States)
Greg Gonzales
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Steven Violette
(Spirit AeroSystems (United States) Wichita, Kansas, United States)
Pat Sullivan
(Spirit AeroSystems (United States) Wichita, Kansas, United States)
Michael Johnson
(Spirit AeroSystems (United States) Wichita, Kansas, United States)
Date Acquired
April 20, 2022
Subject Category
Composite Materials
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR) 2022
Location: Heilbronn
Country: DE
Start Date: June 19, 2022
End Date: June 23, 2022
Sponsors: European Space Agency
Funding Number(s)
WBS: 137271.04.03.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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