A review of technology, history, and current status for pressurized expulsion of cryogenic tankage is presented. Use of tank pressurization to expel cryogenic fluids will continue to be studied for future spacecraft applications over a range of operating conditions in the low-gravity environment. The review examines experimental test results and analytical model development for quiescent and agitated conditions in normal-gravity, followed by a discussion of pressurization and expulsion in low-gravity. Validated, 1-D, finite difference codes exist for the prediction of pressurant mass requirements within the range of quiescent normal-gravity test data. To date, the effects of liquid sloshing have been characterized by tests in normal-gravity...
The paper discusses heat and mass transfer during sloshing of cryogenic liquids. Experiments have be...
This paper presents experimental results for the liquid hydrogen and nitrogen bubble point tests usi...
Technology gaps and system characteristics critical to cryogenic and noncryogenic in-orbit fluid tra...
Requirements are presented for an experiment designed to obtain data for the pressurization and expu...
Experimental results are reported for submerged injection pressurization and expulsion tests of a 4....
Many future space based vehicles and satellites will require on orbit refuelling procedures. Cryogen...
The filling of tanks with cryogens in the low-gravity environment of space poses many technical chal...
There is renewed interest in cryogenic oxygen storage for an advanced second-generation orbital mane...
The tank pressure control experiment is a demonstration of NASA intent to develop new technology for...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76393/1/AIAA-1991-486-786.pd
The literature for tank chilldown methods applicable to cryogenic tankage in the zero gravity enviro...
The no-vent method is a promising approach to handling the problems of low-g venting during propella...
The literature of in-space cryogenic transfer is reviewed in order to propose transportation concept...
In many applications, on-orbit storage and transfer of cryogens will require forced mixing to contro...
NASA Lewis Research has been investigating the no-vent fill method, since it is a promising approach...
The paper discusses heat and mass transfer during sloshing of cryogenic liquids. Experiments have be...
This paper presents experimental results for the liquid hydrogen and nitrogen bubble point tests usi...
Technology gaps and system characteristics critical to cryogenic and noncryogenic in-orbit fluid tra...
Requirements are presented for an experiment designed to obtain data for the pressurization and expu...
Experimental results are reported for submerged injection pressurization and expulsion tests of a 4....
Many future space based vehicles and satellites will require on orbit refuelling procedures. Cryogen...
The filling of tanks with cryogens in the low-gravity environment of space poses many technical chal...
There is renewed interest in cryogenic oxygen storage for an advanced second-generation orbital mane...
The tank pressure control experiment is a demonstration of NASA intent to develop new technology for...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76393/1/AIAA-1991-486-786.pd
The literature for tank chilldown methods applicable to cryogenic tankage in the zero gravity enviro...
The no-vent method is a promising approach to handling the problems of low-g venting during propella...
The literature of in-space cryogenic transfer is reviewed in order to propose transportation concept...
In many applications, on-orbit storage and transfer of cryogens will require forced mixing to contro...
NASA Lewis Research has been investigating the no-vent fill method, since it is a promising approach...
The paper discusses heat and mass transfer during sloshing of cryogenic liquids. Experiments have be...
This paper presents experimental results for the liquid hydrogen and nitrogen bubble point tests usi...
Technology gaps and system characteristics critical to cryogenic and noncryogenic in-orbit fluid tra...