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

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C Design Details <strong>of</strong> Experiment Equipment<br />

portation and 18 ◦ C for preparation at <strong>the</strong> launch site. <strong>During</strong> rocket ascent<br />

<strong>the</strong> skin temperature <strong>of</strong> <strong>the</strong> outer structure rises up to 140 ◦ C, and during reentry<br />

it reaches approximately 200 ◦ C. Never<strong>the</strong>less, <strong>the</strong> temperature <strong>of</strong> <strong>the</strong><br />

DCU within <strong>the</strong> vacuum dome was in <strong>the</strong> order <strong>of</strong> 19 to 33 ◦ C during <strong>the</strong> experimental<br />

phase <strong>of</strong> <strong>the</strong> TEXUS-46 flight. A temperature increase <strong>of</strong> <strong>the</strong> experiment<br />

deck <strong>of</strong> about 6K, due to radiation and suppression <strong>of</strong> convective<br />

cooling, was taken into account for <strong>the</strong> experiment design. An increase from<br />

29 to 32 ◦ C was finally measured for <strong>the</strong> vicinity <strong>of</strong> <strong>the</strong> droplet array generation<br />

device. Depending on <strong>the</strong> winter season in North Sweden, an environmental<br />

temperature <strong>of</strong> −30 ◦ C is probable, but <strong>the</strong> payload temperature after touchdown<br />

does not drop below 0 ◦ C in normal recovery operation, which was <strong>the</strong><br />

case for <strong>the</strong> TEXUS-46 mission.<br />

C.2 Construction and Manufacturing Details<br />

Apart from <strong>the</strong> microgravity environment itself, special design features were<br />

incorporated in <strong>the</strong> experimental setup to provide high quality results. Special<br />

attention was given to <strong>the</strong> droplet array generation system (Fig. 3.2, D) to<br />

realize equal vapor distribution around each droplet as well as a symmetrical<br />

fuel vapor layer around <strong>the</strong> axis <strong>of</strong> <strong>the</strong> droplet array.<br />

Manufacturing <strong>of</strong> Fine Glass Tubes<br />

The manufacturing process <strong>of</strong> <strong>the</strong> fine glass tubes that are integrated into <strong>the</strong><br />

fuel supply block (Fig. 3.4) can be summarized as follows. Commercially obtainable<br />

glass tubes <strong>of</strong> 1mm outer diameter are narrowed down to pairs <strong>of</strong><br />

micropipettes with an outer tip diameter <strong>of</strong> approximately 40µm by a pipette<br />

generator:<br />

220<br />

• Thin-walled glass capillaries <strong>of</strong> standard borosilicate glass are sorted for<br />

outer diameters <strong>of</strong> 0.990±0.002 mm. Their nominal outer and inner diameter<br />

is 1mm and 0.75 mm, respectively. Their length is 90mm.<br />

• A puller is used to vertically stretch <strong>the</strong> selected glass capillaries into<br />

pipettes by applying heat and using <strong>the</strong> gravitational force. If <strong>the</strong> heater

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