Table 9 Experimental studies on cryogenic chill-down
From: Cryogenic propellant management in space: open challenges and perspectives
Reference | Investigation | Gravity Cond. | Fluids | Highlights |
---|---|---|---|---|
Velat92 | Experimental investigation to collect detailed information on flow structure, flow properties, and heat transfer mechanisms associated with cryogenic chill-down. | 1g | Liquid nitrogen | Visualizations of the entire chill-down process are documented among a range of mass fluxes. The existence and magnitude of circumferential and small axial temperature gradients in the transfer line during the various phases of chill-down is reported. |
Hu et al.134 | Liquid nitrogen chill-down rates and flow patterns between upward flow and downward flow in a vertical pipe. | 1g | Liquid nitrogen | Increasing mass flow rate, rewetting temperature, and quench front velocity increase while the critical heat flux decreases. The total chill-down time for upward flow is longer than for downward flow. Critical heat flux, heat transfer coefficient, and the quench front velocity are higher for upward flow. |
Rame and Hartwig135 | Liquid hydrogen chill-down is experimentally studied for continuous and pulsed flow conditions | 1g | Liquid nitrogen | The authors propose a connection between the non-monotonically decreasing temperature and the flow conditions, which increase the heat transfer coefficient. |
Liquid nitrogen chill-down process under both normal gravity and microgravity conditions | 0g, drop tower | Liquid nitrogen | The bottom wall heat flux is lower in 0g than in 1g. Wall temperature and inlet flow rate do depend on gravity. | |
Kawanami et al.101 | Liquid nitrogen forced convective boiling for low mass velocity in terrestrial and microgravity conditions | 1g, 0g | Liquid nitrogen | Heat transfer and quench front velocity is 20% higher in 0g. Gravity has no effect on the maximum heat flux, which increases exponentially with the quench front velocity. |
Hartwig et al.136 | Chill-down in microgravity using pulse flow and low-thermally conductive coatings | Parabolic Flight | Liquid nitrogen | The tested combination of coatings and pulsating flow enhances significantly the performances of the chill-down: 75% reduction of mass consumption. |
Sarae et al.45 | See Table 4. | |||
Kinefuchi et al.46 | See Table 4. |