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Heatshield for Extreme Entry Environment Technology (HEEET) Enabling Missions Beyond Heritage Carbon PhenolicFuture NASA robotic missions utilizing an entry system into Venus and the outer planets, results in extremely high entry conditions that exceed the capabilities of state of the art low to mid density ablators such as PICA or AVCOAT. Previously, mission planners had to assume the use of fully dense carbon phenolic heatshields similar to what was flown on Pioneer Venus or Galileo. Carbon phenolic is a robust TPS material, however, its high density and relatively high thermal conductivity constrain mission planners to steep entries, with high heat fluxes and pressures and short entry durations. The high entry conditions pose challenges for certification in existing ground based test facilities and the longer-term sustainability of CP will continue to pose challenges. NASA has decided to invest in new technology development rather than invest in reviving carbon phenolic. The HEEET project, funded by STMD is maturing a game changing Woven Thermal Protection System technology. HEEET is a capability development project and is not tied to a single mission or destination, therefore, it is challenging to complete ground testing needed to demonstrate a capability that is much broader than any single mission or destination would require. This presentation will status HEEET progress. Near term infusion target for HEEET is the upcoming New Frontiers (NF-4) class of competitively selected Science Mission Directorate (SMD) missions for which it is incentivized.
Document ID
20170010399
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Stackpoole, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Boghozian, T.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Chavez-Garcia, J.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Ellerby, D.
(NASA Ames Research Center Moffett Field, CA, United States)
Fowler, M.
(NASA Johnson Space Center Houston, TX, United States)
Gage, P.
(Neerim Corp. Mountain View, CA, United States)
Gasch, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Gonzales, G.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Kazemba, C.
(NASA Johnson Space Center Houston, TX, United States)
Kellermann, C.
(NASA Langley Research Center Hampton, VA, United States)
Langston, S.
(NASA Langley Research Center Hampton, VA, United States)
Mahzari, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Milos, F.
(NASA Ames Research Center Moffett Field, CA, United States)
Nishioka, O.
(NASA Ames Research Center Moffett Field, CA, United States)
Peterson, K.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Poteet, C.
(NASA Johnson Space Center Houston, TX, United States)
Prabhu, D.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Splinter, S.
(NASA Johnson Space Center Houston, TX, United States)
Venkatapathy, E.
(NASA Ames Research Center Moffett Field, CA, United States)
Williams, J.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Young, Z.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
October 31, 2017
Publication Date
June 26, 2017
Subject Category
Space Sciences (General)
Report/Patent Number
ARC-E-DAA-TN43931
Meeting Information
Meeting: National Space and Missile Materials Symposium (NSMMS) 2017
Location: Indian Wells, CA
Country: United States
Start Date: June 26, 2017
End Date: June 29, 2017
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
thermal protection
carbon phenolic
HEEET
ablators
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