We report the progress in the development of the chilldown model for rapid cryogenic loading system developed at KSC. The nontrivial characteristic feature of the analyzed chilldown regime is its active control by dump valves. The two-phase flow model of the chilldown is approximated as one-dimensional homogeneous fluid flow with no slip condition for the interphase velocity. The model is built using commercial SINDAFLUINT software. The results of numerical predictions are in good agreement with the experimental time traces. The obtained results pave the way to the application of the SINDAFLUINT model as a verification tool for the design and algorithm development required for autonomous loading operation
This is the fourth report in a series of technical reports that describe separated two-phase flow mo...
An extension for cryogenic systems to the AirCondi-tioning Library by Modelon was used to analyze th...
Line Chill-down heat transfer was modelled using SINDA/FLUINT. Multiple chill-down tests were modell...
We report the progress in the development of the chilldown model for a rapid cryogenic loading syste...
We report the progress in the development of the physics based model for cryogenic chilldown and loa...
A cryogenic advanced propellant loading system is currently being developed at NASA. A wide range of...
The timely detection of leaks within cryogenic fuel replenishment systems is of significant importan...
Physics-based approach to the cryogenic flow health management is presented. It is based on fast and...
1. Kennedy Space Center (KSC) is developing a mobile launching system with autonomous propellant loa...
We report on the development of a hierarchy of models of cryogenic two-phase flow motivated by NASA ...
Computer programs were written to model the liquid oxygen loading system for the space shuttle. The ...
We report a development of probabilistic framework for parameter inference of cryogenic two-phase fl...
Line chill-down is an important process in cryogenic tank propellant management, storage, and usage ...
Abstract—The loading of spacecraft propellants is a complex, risky operation. Therefore, diagnostic ...
The literature for tank chilldown methods applicable to cryogenic tankage in the zero gravity enviro...
This is the fourth report in a series of technical reports that describe separated two-phase flow mo...
An extension for cryogenic systems to the AirCondi-tioning Library by Modelon was used to analyze th...
Line Chill-down heat transfer was modelled using SINDA/FLUINT. Multiple chill-down tests were modell...
We report the progress in the development of the chilldown model for a rapid cryogenic loading syste...
We report the progress in the development of the physics based model for cryogenic chilldown and loa...
A cryogenic advanced propellant loading system is currently being developed at NASA. A wide range of...
The timely detection of leaks within cryogenic fuel replenishment systems is of significant importan...
Physics-based approach to the cryogenic flow health management is presented. It is based on fast and...
1. Kennedy Space Center (KSC) is developing a mobile launching system with autonomous propellant loa...
We report on the development of a hierarchy of models of cryogenic two-phase flow motivated by NASA ...
Computer programs were written to model the liquid oxygen loading system for the space shuttle. The ...
We report a development of probabilistic framework for parameter inference of cryogenic two-phase fl...
Line chill-down is an important process in cryogenic tank propellant management, storage, and usage ...
Abstract—The loading of spacecraft propellants is a complex, risky operation. Therefore, diagnostic ...
The literature for tank chilldown methods applicable to cryogenic tankage in the zero gravity enviro...
This is the fourth report in a series of technical reports that describe separated two-phase flow mo...
An extension for cryogenic systems to the AirCondi-tioning Library by Modelon was used to analyze th...
Line Chill-down heat transfer was modelled using SINDA/FLUINT. Multiple chill-down tests were modell...