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Effects of Heat Transfer Coefficient Variation on Nuclear Thermal Propulsion Engine PerformanceA physics-based Nuclear Thermal Propulsion (NTP) Testing Reference Design (TRD) power balance model was coded in Simulink to investigate engine performance for various design and parameter modifications. Since the primary mode of heat transfer in NTP engines is convective, the convective heat transfer coefficient (HTC) is a key parameter that requires accurate representation. The industry standard Westinghouse correlation has an uncertainty of ±20% which was investigated in this study. The results showed that a 20% decrease in the HTC led to a 4.14% increase in maximum fuel temperature while a 20% decrease in the HTC led to a 1.81% decrease in maximum fuel temperature suggesting that narrowing the uncertainty of this correlation through experimental work would be a critical step in the development of NTP engines. Furthermore, a maximum fuel temperature relationship with specific impulse was developed for the TRD engine which showed potential engine operation between specific impulse values of 715 and 900 seconds with minimal changes to the engine design. This graph could be useful for high level vehicle performance estimations for fuel types with different maximum operating temperatures.
Document ID
20230001299
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Daria Nikitaeva
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Corey D. Smith
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Matthew Duchek
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
January 26, 2023
Subject Category
Spacecraft Propulsion and Power
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space (NETS)
Location: Idaho Falls, ID
Country: US
Start Date: May 7, 2023
End Date: May 11, 2023
Sponsors: American Nuclear Society
Funding Number(s)
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Heat Transfer Coefficient
Nuclear Thermal Propulsion
Engine
Uncertainty Analysis
Simulink
SERPENT
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