Abstract
To obtain the detailed heat transfer data and the data concerning directly to the heat transfer mechanisms, i.e. the liquid film thickness underneath attached bubbles, a structure of transparent heating surface was investigated for the TR-IA No. 5 rocket experiment conducted in September, 1996. The sequence of various combinations of system pressure and supplied heat flux level was developed to ensure the boiling initiation, the establishment of experimental conditions for succeeding subdivided phases and the removal of accumulated bubbles. Based on the experimental results and analysis, the summary and comments about the experimental hardware, the sequence of system parameters varied, the structure of coalesced bubble are presented as the first report for the purpose of the improvement of further studies in the same research field.