Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX17CS03C
Agency Tracking Number: 156333
Amount: $750,000.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: H10.02
Solicitation Number: N/A
Solicitation Year: 2016
Award Year: 2017
Award Start Date (Proposal Award Date): 2017-04-19
Award End Date (Contract End Date): 2019-04-18
Small Business Information
420 Park Avenue West, Princeton, IL, 61356-1934
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Rex Chamberlain
 Principal Investigator
 (815) 872-0702
Business Contact
 Rex Chamberlain
Title: Business Official
Phone: (815) 872-0702
Research Institution
Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as pumps, turbines, valves and chokes may experience vibration and damage due to cavitation in the flowing liquid, and any reduction in the severity of the operating conditions would provide expanded test and performance benefits. The proposed innovation is to develop an unsteady cavitation model based on a tabular equation of state and a representation of cavitation bubble dynamics that together describe the growth and collapse of nucleated bubbles in a liquid cryogen. Important nonequilibrium mechanical and thermal effects will be considered by using a drift-flux model and adding an additional energy equation for the liquid temperature. Validation of the advanced cavitation models will be accomplished for both steady and unsteady flows by comparing surface pressure and temperature data and computing power spectra from frequency domain analyses. The final analysis tool will be used to demonstrate the significant nonequilibrium flow behavior for both the validation cases and actual production analysis problems of interest to NASA.

* Information listed above is at the time of submission. *

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