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Table 4 Temperature-dependent heat transfer coefficient at the hot side of the copper liner (Kowollik 2015)

From: Stress evolution in thermal barrier coatings for rocket engine applications

Temperature / K Heat transfer / Wm−2K−1
70 53779
167 55244
348 54881
562 52877
748 50754
873 49326
937 48637
962 48404
968 48354
969 48349
1031 47623
1138 46374
1259 45004
1361 43901
1427 43235
1461 42941
1474 42849
1477 42830
1478 42827