Publication Date:
2019-07-13
Description:
Heat transfer rate measurements have been obtained at 0, 5, 15, and 21 deg angles-of-attack for a straight biconic scale model of an aeroassisted orbital vehicle proposed for planetary probe missions. Heat-transfer distributions were measured using palladium thin-film resistance gauges deposited on a glass-ceramic substrate. The windward heat transfer correlations were based on equilibrium flow in the shock layer of the model, although the flow may depart from equilibrium in the flow-field.
Keywords:
ASTRONAUTICS (GENERAL)
Type:
ICAS Congress; Aug 28, 1988; Jerusalem; Israel
Format:
text
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