Europa Clipper Thermal Control Valve Thermal and Hydraulic Analysis and Development Testing

dc.creatorKandilian, Razmig
dc.creatorBhandari, Pradeep
dc.creatorMastropietro, Arthur
dc.creatorZhang, Conan
dc.creatorCarroll, Brian
dc.date.accessioned2019-06-26T14:07:38Z
dc.date.available2019-06-26T14:07:38Z
dc.date.issued2019-07-07
dc.descriptionRazmig Kandilian, Jet Propulsion Laboratory (JPL), USA
dc.descriptionPradeep Bhandari, Jet Propulsion Laboratory (JPL), USA
dc.descriptionArthur Mastropietro, Jet Propulsion Laboratory (JPL), USA
dc.descriptionConan Zhang, Jet Propulsion Laboratory (JPL), USA
dc.descriptionBrian Carroll, Jet Propulsion Laboratory (JPL), USA
dc.descriptionICES101: Spacecraft and Instrument Thermal Systems
dc.descriptionThe 49th International Conference on Environmental Systems as held in Boston, Massachusetts, USA on 07 July 2019 through 11 July 2019.
dc.description.abstractThis manuscript describes the thermal and hydraulic analysis performed on Europa Clipper heat recovery system (HRS) thermal control valves as well as a radiation test to reduce risk of hardware failure during the mission. Europa Clipper is a solar powered mission to Jupiter where solar irradiance can be as low as 48 W/m2. The spacecraft also flies by Venus for gravity assist where the solar irradiance can reach 3300 W/m2. The spacecraft thermal design requires 1) the conservation of maximum amount of heat possible near Jupiter and 2) rejection of large amounts of heat during the Venus flyby. To achieve this, the HRS employs two JPL heritage thermal control valves in series to modulate flow to the radiator between 2.4 ml/min and 1.3 LPM. The thermal and hydraulic analysis were key in determining flow rate to the radiator as a function of fluid temperature in order to predict spacecraft temperatures. Hydraulic analysis was also performed to determine leak paths between the block redundant pairs of the thermal control valves. Finally, a development test was undertaken to determine the effects of ionizing radiation on the performance of the thermal control valve. The valve was exposed to a total ionizing dose of 300 krad, the maximum expected dose in the Clipper Vault. The flow characteristics of the valve was performed as a function of temperature before and after radiation exposure to determine ionizing radiation impact on valve performance.
dc.format.mimetypeapplication/pdf
dc.identifier.otherICES_2019_42
dc.identifier.urihttps://hdl.handle.net/2346/84725
dc.language.isoeng
dc.publisher49th International Conference on Environmental Systems
dc.subjectThermal control systems
dc.subjectthermal control valve
dc.subjectionizing radiation
dc.subjectheat rejection system
dc.subjecthydraulic analysis
dc.subjectmechanically pumped fluid loop
dc.subjectsingle phase
dc.subjectEuropa Clipper
dc.titleEuropa Clipper Thermal Control Valve Thermal and Hydraulic Analysis and Development Testingen_US
dc.typePresentations

Files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
ICES-2019-42.pdf
Size:
760.91 KB
Format:
Adobe Portable Document Format
Description:

License bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.57 KB
Format:
Item-specific license agreed upon to submission
Description: