Abstract
Laboratory studies were conductd to increase the use temperature capability of coatings for Silica Reusable Surface Insulation. The approach for this aspect of improved coating studies under NAS2-9809 is based on increasing the viscosity at the re-entry temperature to more adequately resist the aerodynamic shear forces experienced during entry from Earth orbits. The methods used to increase coating viscosity while maintaining current processing techniques and sintering schedules were: (1) reduction in the concentration of the relatively low viscosity additive, B//2O//3; (2) reduction in the particle size of the constituent powders used in making the coatings; and (3) addition of a relatively high viscosity glass former (GeO//2). In combining all three methods, a coating system was identified that showed apparent higher viscosity than the current coating while satisfying all the current Shuttle Orbiter Coating requirements.
| Original language | English |
|---|---|
| Title of host publication | National SAMPE Technical Conference |
| Publisher | SAMPE (v 11) |
| Pages | 114-124 |
| Number of pages | 11 |
| Publication status | Published - 1979 |
| Event | Natl SAMPE Tech Conf 11th, New Horiz - Mater and Processes for the Eighties - Boston, Mass Duration: Nov 13 1979 → Nov 15 1979 |
Other
| Other | Natl SAMPE Tech Conf 11th, New Horiz - Mater and Processes for the Eighties |
|---|---|
| City | Boston, Mass |
| Period | 11/13/79 → 11/15/79 |
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ASJC Scopus subject areas
- Engineering(all)
Cite this
DEVELOPMENT OF HIGH VISCOSITY COATINGS FOR ADVANCED SPACE SHUTTLE APPLICATIONS. / Garofalini, Steve; Banas, R.; Creedon, J.
National SAMPE Technical Conference. SAMPE (v 11), 1979. p. 114-124.Research output: Chapter in Book/Report/Conference proceeding › Chapter
}
TY - CHAP
T1 - DEVELOPMENT OF HIGH VISCOSITY COATINGS FOR ADVANCED SPACE SHUTTLE APPLICATIONS.
AU - Garofalini, Steve
AU - Banas, R.
AU - Creedon, J.
PY - 1979
Y1 - 1979
N2 - Laboratory studies were conductd to increase the use temperature capability of coatings for Silica Reusable Surface Insulation. The approach for this aspect of improved coating studies under NAS2-9809 is based on increasing the viscosity at the re-entry temperature to more adequately resist the aerodynamic shear forces experienced during entry from Earth orbits. The methods used to increase coating viscosity while maintaining current processing techniques and sintering schedules were: (1) reduction in the concentration of the relatively low viscosity additive, B//2O//3; (2) reduction in the particle size of the constituent powders used in making the coatings; and (3) addition of a relatively high viscosity glass former (GeO//2). In combining all three methods, a coating system was identified that showed apparent higher viscosity than the current coating while satisfying all the current Shuttle Orbiter Coating requirements.
AB - Laboratory studies were conductd to increase the use temperature capability of coatings for Silica Reusable Surface Insulation. The approach for this aspect of improved coating studies under NAS2-9809 is based on increasing the viscosity at the re-entry temperature to more adequately resist the aerodynamic shear forces experienced during entry from Earth orbits. The methods used to increase coating viscosity while maintaining current processing techniques and sintering schedules were: (1) reduction in the concentration of the relatively low viscosity additive, B//2O//3; (2) reduction in the particle size of the constituent powders used in making the coatings; and (3) addition of a relatively high viscosity glass former (GeO//2). In combining all three methods, a coating system was identified that showed apparent higher viscosity than the current coating while satisfying all the current Shuttle Orbiter Coating requirements.
UR - http://www.scopus.com/inward/record.url?scp=0018735566&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0018735566&partnerID=8YFLogxK
M3 - Chapter
AN - SCOPUS:0018735566
SP - 114
EP - 124
BT - National SAMPE Technical Conference
PB - SAMPE (v 11)
ER -