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Dataset: Bubble Free Cryogenic Liquid Acquisition Device, Phase I
Provided by National Aeronautics and Space Administration
Updated 12 Nov 2020

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Dataset summary

The dataset on this page is a cache of the dataset https://catalog.data.gov/dataset/bubble-free-cryogenic-liquid-acquisition-device-phase-i. It is a snapshot of the dataset as it appeared on 06 Jun 2021 21:03 GMT. The current dataset could have changed in the meantime. Attribution: Contains data retrieved from Data.gov.

Recent results of fundamental capillary fluidics investigations conducted aboard the ISS have targeted families of geometries with direct application to Liquid Acquisition Devices for low-g propellant management. NASA's exploration goals will demand low-g cryogenic propellant management for the Exploration Upper Stage and other vehicles. The specific geometric requirements of a LAD providing bubble-free cryogenic rocket engine flows of 37L/min may now be readily determined using closed-form expressions validated from archived ISS investigations. In this effort we provide the precise geometric specifications and margins for a passive capillary fluidic LAD for cryogenic fluid management for in-space transportation. We will provide design tools such that dimensions may be tuned to adapt to changes in requirements, propellants, tank geometry, materials, flight, etc. We will employ the SE-FIT software to determine all a/symmetric global minimizing surfaces and myriad stability limits as fun...

Dataset:Bubble Free Cryogenic Liquid Acquisition Device, Phase I
Provider:National Aeronautics and Space Administration
Created:12/11/2020
Updated:12/11/2020
Licence:License information is derived automatically. Refer to source for license information before using this data.
notspecified
License not specified
Country:United States of America

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