NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Demonstration of the range over which the Langley Research Center digital computer charring ablation program (CHAP) can be used with confidence: Comparisons of CHAP predictions and test data for three ablation materialsComparisons of ablation calculations with the charring ablation computer code and ablation test data are presented over a wide range of environmental conditions in air for three materials: low-density nylon phenolic, Avcoat 5026-39HC/G, and a filled silicon elastomer. Heat fluxes considered range from over 500 Btu/sq ft-sec to less than 50 Btu/sq ft-sec. Pressures range from 0.5 atm to .004 atm. Enthalpies range from about 2000 Btu/lb to 18000 Btu/lb. Predictions of recession, pyrolysis penetration, and thermocouple responses are considered. Recession predictions for nylon phenolic are good as steady state is approached, but strongly transient cases are underpredicted. Pyrolysis penetrations and thermocouple responses are very well predicted. Recession amounts for Avcoat and silicone elastomer are less well predicted, although high heat flux cases near steady state are fairly satisfactory. Pyrolysis penetrations and thermocouple responses are very well predicted.
Document ID
19720011302
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moyer, C. B.
(Aerotherm Corp. Mountain View, CA, United States)
Green, K. A.
(Aerotherm Corp. Mountain View, CA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1972
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-1980
REPT-71-35
Report Number: NASA-CR-1980
Report Number: REPT-71-35
Accession Number
72N18952
Funding Number(s)
CONTRACT_GRANT: NAS1-10136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available