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Using Tapered Channels to Improve LAD Performance for Cryogenic Fluids: Suborbital Testing Results

Kevin Supak

Kevin Supak

Southwest Research Institute®San Antonio,
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Supak, Kevin
, 
Steve Green

Steve Green

Southwest Research Institute®San Antonio,
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Green, Steve
 und 
Amy McCleney

Amy McCleney

Southwest Research Institute®San Antonio,
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McCleney, Amy
  
26. Juni 2021
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Artikel-Kategorie: Research Note
Online veröffentlicht: 26. Juni 2021
Seitenbereich: 115 - 120
DOI: https://doi.org/10.2478/gsr-2021-0009
Schlüsselwörter
© 2021 Kevin Supak et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Figure 1

Liquid acquisition device illustration for storable propellants.
Liquid acquisition device illustration for storable propellants.

Figure 2

Tapered liquid acquisition device concept for cryogenic propellants.
Tapered liquid acquisition device concept for cryogenic propellants.

Figure 3

Photograph of bubble migration in a tapered liquid acquisition device.
Photograph of bubble migration in a tapered liquid acquisition device.

Figure 4

Ground test data for a 5° tapered liquid acquisition device.
Ground test data for a 5° tapered liquid acquisition device.

Figure 5

Photograph of the tapered liquid acquisition devices for the first flight experiment.
Photograph of the tapered liquid acquisition devices for the first flight experiment.

Figure 6

Microgravity test data as compared with ground test data.
Microgravity test data as compared with ground test data.

Figure 7

Photograph of the tapered liquid acquisition devices for the second flight experiment.
Photograph of the tapered liquid acquisition devices for the second flight experiment.
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Englisch
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