We report on the development of a hierarchy of models of cryogenic two-phase flow motivated by NASA plans to develop and maturate technology of cryogenic propellant loading on the ground and in space. The solution of this problem requires models that are fast and accurate enough to identify flow conditions, detect faults, and to propose optimal recovery strategy. The hierarchy of models described in this presentation is ranging from homogeneous moving- front approximation to separated non-equilibrium two-phase cryogenic flow. We compare model predictions with experimental data and discuss possible application of these models to on-line integrated health management and control of cryogenic loading operation
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A cryogenic advanced propellant loading system is currently being developed at NASA. A wide range of...
We report the progress in the development of the physics based model for cryogenic chilldown and loa...
We report the progress in the development of the chilldown model for rapid cryogenic loading system ...
Physics-based approach to the cryogenic flow health management is presented. It is based on fast and...
We report the progress in the development of the chilldown model for a rapid cryogenic loading syste...
Abstract—The loading of spacecraft propellants is a complex, risky operation. Therefore, diagnostic ...
We report a development of probabilistic framework for parameter inference of cryogenic two-phase fl...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
1. Kennedy Space Center (KSC) is developing a mobile launching system with autonomous propellant loa...
The purpose of this report is to provide a summary of state-of-the-art predictions for two-phase flo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A cryogenic advanced propellant loading system is currently being developed at NASA. A wide range of...
We report the progress in the development of the physics based model for cryogenic chilldown and loa...
We report the progress in the development of the chilldown model for rapid cryogenic loading system ...
Physics-based approach to the cryogenic flow health management is presented. It is based on fast and...
We report the progress in the development of the chilldown model for a rapid cryogenic loading syste...
Abstract—The loading of spacecraft propellants is a complex, risky operation. Therefore, diagnostic ...
We report a development of probabilistic framework for parameter inference of cryogenic two-phase fl...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
During the ballistic phase of a cryogenic upper stage, attitude and orbit control are usually perfor...
1. Kennedy Space Center (KSC) is developing a mobile launching system with autonomous propellant loa...
The purpose of this report is to provide a summary of state-of-the-art predictions for two-phase flo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...
A lumped-parameter computational simulation is developed, tested, and used to model a non-vented slo...