Cited by 4Spacecraft and Cryogenic TechnologiesHeat Transfer and Boiling StudiesHeat transfer and supercritical fluids

Thermal Modeling of Zero Boil Off Tank Experiment

Open access
Tesny, Erin M., Hauser, Daniel M.·2019·AIAA Propulsion and Energy 2019 Forum

Abstract

Understanding fluid behavior in microgravity environments is essential to further development of cryogenic storage in space environments. The Zero Boil Off Tank (ZBOT) experiment was designed to investigate two-phase pressurization and depressurization of a tank in a microgravity environment. The test fluid was the refrigerant Perfluoro-normal-Pentane (PNP). Thermal modeling for the ZBOT model was conducted using Thermal Desktop and SINDA/FLUINT. The temperature distribution within the fluid of the tank is of particular interest. This particular work is centered on ascertaining the thermal behavior of the refrigerant in order to build more complete models of fluid in microgravity. Separate cases were run modeling experiments that were conducted both on the ground and on the International Space Station (ISS) to compare 1g and microgravity environments. The microgravity modeling cases consisted of a fluid lump representing the vapor ullage suspended in a solid to represent the liquid. Mass flow between the liquid and vapor was modeled using the Schrage equation for mass flow. Initial results indicate that the pressure rise and temperature increase within the fluid closely align with the experimental data by matching initial conditions of the experiment. This work is ongoing and will yield further insights into the thermal behavior of fluid mixing in microgravity.

The claims and statistics of this paper haven’t been checked yet.

Run the check — free, no account needed. It reads the open-access text and checks the sources it cites.

A few free checks a day · papers already verified open instantly · results are public

Integrity signals

Registry

Crossref · 10.2514/6.2019-4280

Cites

Statistics

Claims the paper makes

The claims and statistics of this paper haven’t been checked yet.

Run the check — free, no account needed. It reads the open-access text and checks the sources it cites.

A few free checks a day · papers already verified open instantly · results are public

Claims other papers make about this one

Each is checked against this paper’s own text: does it say what the citing paper says it does?

  • This capability of the model to simulate storage at sub-atmospheric pressures is highly relevant to LH2 applications in microgravity environments, including the cryogenic storage systems needed for future long-term space missions.

    “This capability of the model to simulate storage at sub-atmospheric pressures is highly relevant to LH 2 applications in microgravity environments, including the cryogenic storage systems needed for future long-term space missions [90].”

    From Modelling of Liquid Hydrogen Boil-Off (2022) · cites this paper as [90]

    The Background (page unavailable) says cryogenic-fluid storage in microgravity is crucial for future long-term space missions, and Future Work proposes comparing the model’s results with a cryogen in microgravity. Our copy does not establish that the model can simulate storage at sub-atmospheric pressures or specifically address LH2; the experiment used perfluoro-normal-pentane. (LLM, conf=0.84)

    Experimental — accuracy not yet measured

Self-check

Percentages, sums and reported differences re-computed from the paper’s own numbers.

The self-check needs the paper’s full text.

Cited by

Sorted by citations

Authors
Tesny, E. M., & Hauser, D. M.
Affiliations
Glenn Research Center (US)
Venue
AIAA Propulsion and Energy 2019 Forum
Published
2019-08-16
OpenAlex
W2967229613
Cited by
4
References
0
Citations by year
2026: 1 · 2024: 1 · 2023: 1 · 2022: 1
FWCI
0.45
Type
conference paper
Language
en
Open access
Locations
  • AIAA Propulsion and Energy Forum (publishedVersion)
  • NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
Funders
  • Case Western Reserve University
  • Space Technology Mission Directorate
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft and Cryogenic Technologies
  • Physical Sciences › Engineering › Mechanical Engineering › Heat Transfer and Boiling Studies
  • Physical Sciences › Engineering › Computational Mechanics › Heat transfer and supercritical fluids
Keywords
cryogenic storage, microgravity, depressurization, International Space Station, thermal modeling, SINDA/FLUINT, fluid mixing

About these checks

Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

Statistics and arithmetic are recomputed, not judged.

Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.

What counts as a claim ›How we measure confidence ›How we check this ›

Are you an author, or do you see a problem with this page? Request a review