Table 2 Experimental conditions for the six flight cases.

From: Cryogenic spray quenching of simulated propellant tank wall using coating and flow pulsing in microgravity

Case

Pin (psig)

Duty cycle (%)

Period (second)

g-level

1

80

100

NA

microgravity

2

80

40

1

microgravity

3

80

70

1

microgravity

4

60

100

NA

microgravity

5

90

100

NA

microgravity

6

90

50

1

microgravity

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