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On the Formation of Nitrogen Oxides During the Combustion of ...

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3.2 Measurement Techniques and Data Acquisition<br />

Table 3.9: Nominal Experiment Parameters for Droplet Arrays on TEXUS-46. The droplet<br />

number is N = 5, and <strong>the</strong> non-dimensionless droplet spacing S = 18mm [195].<br />

Pre-vaporization Droplet diameter Dimensionless<br />

No. time t Ψ in s initial D 0 in mm ignition D ign in mm spacing ratio S/D ign<br />

1 18 1.5 1.01 17.8<br />

2 10 1.5 1.34 13.4<br />

3 5 1.5 1.47 12.2<br />

4 15 1.5 1.15 15.7<br />

from repeated countdown holds during <strong>the</strong> final steps <strong>of</strong> <strong>the</strong> TEXUS launch<br />

sequence. Apart from testing and validation, <strong>the</strong> experiments <strong>of</strong> <strong>the</strong> TEXNOX<br />

drop tower campaign were destined to diversify <strong>the</strong> scientific output. Here,<br />

<strong>the</strong> initial droplet diameter D 0 was varied in <strong>the</strong> range <strong>of</strong> 0.8 to 1.0mm, a dimensionless<br />

spacing ratio S/D 0 <strong>of</strong> 4.5, 6.0, and 9.0 with 17, 13, and 9 droplets<br />

was applied (Tab. 3.1), and preheating temperature T Ψ was set at 300, 400, 450,<br />

and 500 K. The different amounts <strong>of</strong> pre-vaporization time t Ψ and preheating<br />

temperature T Ψ were essential for <strong>the</strong> development <strong>of</strong> a flammable gas layer<br />

around <strong>the</strong> droplets and for diversification [195–197, 208, 293, 294, 296].<br />

Control <strong>of</strong> Droplet Lifting System<br />

The droplet lifting system moves <strong>the</strong> droplet array holder 105 mm vertically<br />

from its initial position to <strong>the</strong> end position inside <strong>the</strong> combustion chamber.<br />

Stepper motor, gear system, and crank arms are adjusted for a quick<br />

but smooth operation. The working time for covering <strong>the</strong> distance <strong>of</strong> 105 mm<br />

was set to 2.0s for <strong>the</strong> TEXUS-46 sounding rocket flight but to 1350 ms for <strong>the</strong><br />

TEXNOX drop tower campaign due to <strong>the</strong> limited microgravity time. Fur<strong>the</strong>rmore,<br />

<strong>the</strong> lift-up process was started 700ms before <strong>the</strong> drop capsule release<br />

to extend <strong>the</strong> available time for droplet burnout within <strong>the</strong> drop tower experiments<br />

(cf. Fig. 3.18). This approach split <strong>the</strong> process into two phases: a first<br />

phase under normal gravity with <strong>the</strong> droplet array in ambient temperature<br />

T ∞ and a second phase under microgravity with <strong>the</strong> droplet array exposed to<br />

<strong>the</strong> preheated combustion chamber. Bringing forward <strong>the</strong> lift-up process fur<strong>the</strong>r<br />

is limited by <strong>the</strong> abrupt drop <strong>of</strong> surface tension during <strong>the</strong> temperature<br />

101

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