发明名称 Adjustable high emittance gap filler
摘要 A flexible, adjustable refractory filler (1) is disclosed for filling gaps between ceramic tiles (10, 11) forming the heat shield of a space shuttle vehicle, to protect its aluminum skin (20) during atmospheric re-entry. The easily installed and replaced filler (1) consists essentially of a strip of ceramic cloth (3) coated, at least along both its longitudinal edges (4, 5), with a room temperature vulcanizable silicone rubber compound with a high emittance colored pigment. The filler may have one or more layers (2, 3), as the gap width requires. Preferred materials are basket-weave aluminoborosilicate cloth, and a rubber compounded with silicon tetraboride as the emittance agent and finely divided borosilicate glass containing about 7.5% B2O3 as high temperature binder. The filler cloth strip or tape is cut to proper width and length, inserted into the gap, and fastened with previously applied drops of silicone rubber adhesive.
申请公布号 US4308309(A) 申请公布日期 1981.12.29
申请号 US19800147700 申请日期 1980.05.07
申请人 FROSCH, ROBERT A. ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WITH RESPECT TO AN INVENTION OF;LEISER, DANIEL B.;STEWART, DAVID A.;SMITH, MARNELL;ESTRELLA, CARLOS A.;GOLDSTEIN, HOWARD E. 发明人 FROSCH, ROBERT A. ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WITH RESPECT TO AN INVENTION OF;LEISER, DANIEL B.;STEWART, DAVID A.;SMITH, MARNELL;ESTRELLA, CARLOS A.;GOLDSTEIN, HOWARD E.
分类号 B64G1/50;B64G1/58;F42B15/34;(IPC1-7):B32B23/02;F42B11/00 主分类号 B64G1/50
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