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Development Testing and Analysis of the Integrated Gateway-ESPRIT Bipropellant Refuelling SystemThe Gateway will be humanity’s first space station orbiting the Moon completed by NASA in partnership with ESA and other US and international partners. The Gateway will provide critical support to sustainable human exploration on the moon through the Artemis program. To enable the Lunar Gateway to complete its mission, on orbit refuelling is essential. The ESPRIT Refuelling Module (ERM) will provide the capability to transfer propellants, MMH and MON-3, through the Habitation and Logistics Outpost (HALO) to the Power and Propulsion Element (PPE). The transfer of these propellants carries known risks and hazards. These hazards include overpressure of the propellant lines during priming sequences between modules and during refuelling pause operations. To support the early system development and to mitigate these risks, a collaborative test program between NASA, ESA and Thales Alenia Space was completed at the Thales Alenia Space test facility in Harwell, UK. This test program integrated fluidic breadboards of the ERM, HALO and PPE modules. The objectives of the test program were to demonstrate and characterise critical performance and transient operations, inform refuelling concept of operations and to calibrate and validate numerical models of the refuelling subsystem in EcosimPro. To support the completion of this final objective a detailed model of the integrated breadboard was developed in EcosimPro and key steady-state and transient test cases were simulated. As an industry first, a National Institute of Standards and Technology (NIST) database correlation for Hydrofluoroether (HFE-7000) was used as a mixed oxides of nitrogen (MON-3) simulant with EcosimPro and European Space Propulsion System Simulation (ESPSS) libraries to result in a more accurate analysis for transient phenomenon such as priming. The test and simulation data showed good agreement validating the model for further system analysis as the ERM design progresses.
Document ID
20240004586
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Andrew Francis Hughes
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Kiran Pazhayattinkal
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Isheeta Ranade
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Abhijit Pandit
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
William Harper
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Alex Millington-Cotes
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Avichai Elimelech
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Lahib Balika
(Thales Alenia Space (United Kingdom) Reading, Berkshire, United Kingdom)
Olivier Zagoni
(Thales Alenia Space (France) Cannes, France)
Alexandra Bulit
(European Space Research and Technology Centre Noordwijk-Binnen, Netherlands)
Adela Han
(Jacobs (United States) Dallas, Texas, United States)
Brian Lusby
(Johnson Space Center Houston, United States)
Pooja Desai
(Johnson Space Center Houston, United States)
Chris Radke
(Johnson Space Center Houston, United States)
Date Acquired
April 15, 2024
Publication Date
May 20, 2024
Subject Category
Propellants And Fuels
Spacecraft Propulsion and Power
Report/Patent Number
SP2024_457
Meeting Information
Meeting: 9th Edition of the 3AF International Conference on Space Propulsion
Location: Glasgow
Country: GB
Start Date: May 20, 2024
End Date: May 23, 2024
Sponsors: Association Aéronautique et Astronautique de France, Centre National d'Études Spatiales, United Kingdom Space Agency, European Space Agency
Funding Number(s)
WBS: 651937.06.03.72
CONTRACT_GRANT: ESA 1550006780
CONTRACT_GRANT: 80JSC022DA035
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Refuelling
Bipropellants
Breadboard Test
Analysis
Verification and Validation
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