Rocket Engine Health Management System - Turbopump System

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$749,590.00
Award Year:
2006
Program:
SBIR
Phase:
Phase II
Contract:
FA9300-06-C-1006
Agency Tracking Number:
F051-201-1698
Solicitation Year:
2005
Solicitation Topic Code:
AF05-201
Solicitation Number:
2005.1
Small Business Information
TURBO SOLUTIONS ENGINEERING LLC
PO Box 722 16 Beaver Meadow Road, Norwich, VT, 05055
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
169816837
Principal Investigator:
Nicholas D'Orsi
Managing Partner, Chief E
(802) 649-8710
ndorsi@turbosoleng.com
Business Contact:
Chip Hobson
Managing Partner, Project
(802) 649-8710
chobson@turbosoleng.com
Research Institution:
n/a
Abstract
Turbo Solutions Engineering LLC is providing this proposal for a Phase II Small Business Innovation Research (SBIR) program, to develop a rocket engine health management (REHM) system. The proposed project is a follow-on to Turbo Solutions’ nearly completed Phase I SBIR entitled “Integrated Vehicle Health Management ‘Intelligent Engine’ Turbopump Concept,” (AFRL Contract FA9300-05-M-3011). We envision coordinating our Phase II effort with WASK Engineering, Inc. (WASK). Turbo Solutions would execute this turbomachinery-focused Phase II SBIR, and WASK would carry out their Phase II SBIR that is focused on the engine system. This coordinated team approach would create a REHM concept that meets AFRL objectives to develop an overall vehicle health management philosophy for use in future engine development programs. The primary application for this REHM system would be the Integrated Powerhead Demonstrator (IPD), although the concept that is developed would be applicable to other engine cycles. The technical objectives are to develop a turbopump model for the IPD that includes the pumps, turbines, and secondary flow systems; integrate this model with the engine system ROCETS model being developed by WASK; and “train” this integrated model to detect, identify, and categorize failures throughout the IPD engine system using a recommended sensor suite.

* information listed above is at the time of submission.

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