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Turbopump Design for Deep Throttling Capability
Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CB78C
Agency Tracking Number: 070083
Amount:
$599,989.00
Phase:
Phase II
Program:
STTR
Solicitation Topic Code:
T8.02
Solicitation Number:
N/A
Timeline
Solicitation Year:
2007
Award Year:
2009
Award Start Date (Proposal Award Date):
2009-09-29
Award End Date (Contract End Date):
2013-03-29
Small Business Information
6325 West 55th
Arvada, CO
80002-2777
United States
DUNS:
074072554
HUBZone Owned:
No
Woman Owned:
No
Socially and Economically Disadvantaged:
No
Principal Investigator
Name: JUDY BUSBY
Title: Principal Investigator
Phone: (303) 421-8111
Email: JBUSBY@BARBER-NICHOLS.COM
Title: Principal Investigator
Phone: (303) 421-8111
Email: JBUSBY@BARBER-NICHOLS.COM
Business Contact
Name: Tim Miller
Title: Business Official
Phone: (303) 303-8111
Email: tmiller@barber-nichols.com
Title: Business Official
Phone: (303) 303-8111
Email: tmiller@barber-nichols.com
Research Institution
Name: The University of Alabama in Huntsville
Contact: Not Available
Address:
Phone: (256) 824-6000
Type: Domestic Nonprofit Research Organization
Contact: Not Available
Address:
301 Sparkman Drive
Huntsville, AL
35899
United States
Phone: (256) 824-6000
Type: Domestic Nonprofit Research Organization
Abstract
This project will demonstrate the benefits of a partial emission pump coupled with a zero net positive suction pressure inducer design to achieve robust, deep throttling capability. This pump application is well suited for 5k to 15k lbf thrust range rocket engines.
* Information listed above is at the time of submission. *
