A Study on the Thermal Analysis and Insulation of KSR-III

2000 
Thermal analysis of KSR-III has been studied to calculate the surface heat transfer and temperature, with which thermal safety of rocket structures is investigated. In the present study, the honeycomb sandwich structure of nose fairing, which is one of the typical multi-layer structures of KSR-III, is thermally analyzed. In addition, the fin tip roll thruster case is thermally analyzed, considering aerodynamic heating, radiation from rocket plume and prelaunch heating concurrently. Some parts of structures are insulated to thermally protect the surface itself and inner payloads.
    • Correction
    • Source
    • Cite
    • Save
    • Machine Reading By IdeaReader
    0
    References
    1
    Citations
    NaN
    KQI
    []