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Visco jet joule-thomson device characterization tests in liquid methane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jurns, John M. |
| Copyright Year | 2009 |
| Description | Joule-Thomson (J-T) devices have been identified as critical components for Thermodynamic Vent Systems (TVS) planned for future space exploration missions. Lee Visco Jets (The Lee Company) (Ref. 4) are one type of J-T device that may be used for LCH4 propellant systems. Visco Jets have been previously tested and characterized in LN2 and LH2 (Refs. 6 and 7), but have not been characterized in LOX or LCH4. Previous Visco Jet tests with LH2 resulted in clogging of the Visco Jet orifice under certain conditions. It has been postulated that this clogging was due to the presence of neon impurities in the LH2 that solidified in the orifices. Visco Jets therefore require testing in LCH4 to verify that they will not clog under normal operating conditions. This report describes a series of tests that were performed at the NASA Glenn Research Center to determine if Visco Jets would clog under normal operating conditions with LCH4 propellant. Test results from this program indicate that no decrease in flow rate was observed for the Visco Jets tested, and that current equation used for predicting flow rate appears to under-predict actual flow at high Lohm ratings. |
| File Size | 2731763 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20090015375 |
| Archival Resource Key | ark:/13960/t4qk2d87z |
| Language | English |
| Publisher Date | 2009-03-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Methane Performance Tests Joule-thomson Effect Propulsion System Performance Liquefied Gases Blocking Characterization Thermodynamics Contaminants Vents Orifices Flow Velocity Mass Flow Cryogenic Rocket Propellants Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |