Development of Engine Loads Methodology

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX11CH34P
Agency Tracking Number: 105123
Amount: $99,720.00
Phase: Phase I
Program: SBIR
Awards Year: 2011
Solicitation Year: 2010
Solicitation Topic Code: X2.01
Solicitation Number: N/A
Small Business Information
11995 El Camino Real, Suite 200, San Diego, CA, -
DUNS: 133709001
HUBZone Owned: N
Woman Owned: Y
Socially and Economically Disadvantaged: N
Principal Investigator
 Eric Blades
 Principal Investigator
 (256) 325-1116
 eric.blades@ata-e.com
Business Contact
 Ronan Cunningham
Title: Business Official
Phone: (858) 480-2015
Email: ronan.cunningham@ata-e.com
Research Institution
 Stub
Abstract
This SBIR seeks to improve the definition of design loads for rocket engine components such that higher performing, lighter weight engines can be developed more quickly. The long-term goal of this SBIR program is to substantially improve the overall load determination by demonstrating and validating new methods. The overall plan includes advances in computational fluid mechanics to provide more accurate tools for estimating the nozzle side loads and fluctuating pressure loads as well as the interaction between system models and components models and the combination of dynamic loads for prediction of component margins and life. The Phase I detailed development includes a tightly-integrated coupling of computational fluid dynamics and structural dynamics codes to better predict the nozzle side loads due to flow separation. In addition, improvements will be identified to both the loads process and the combination of dynamic loads in the time domain to support finite fatigue life predictions. These improvements to the loads definition will provide an improvement to the engine development process by providing better loads estimations which can be used to reduce conservatism and to significantly improve performance with reduced weight, cost, and development time. Phase II will include efforts to validate the fluid-structure interaction tool with experimental data and further develop and validate the new loads process methodologies.

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

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