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Low-Cost Manufacturing Technique for Advanced Regenerative Cooling for In-Space Cryogenic Engines

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CC33P
Agency Tracking Number: 125393
Amount: $124,436.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: H2.02
Solicitation Number: N/A
Timeline
Solicitation Year: 2012
Award Year: 2013
Award Start Date (Proposal Award Date): 2013-05-23
Award End Date (Contract End Date): 2013-11-23
Small Business Information
AL
Huntsville, AL 35806-3200
United States
DUNS: 839422763
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Thomas Haymond
 Principal Investigator
 (256) 562-2157
 Thomas.haymond@asi-hsv.com
Business Contact
 Sandra Fossett
Title: Contracts Administrator
Phone: (256) 562-2165
Email: Sandra.Fossett@asi-hsv.com
Research Institution
 Stub
Abstract

The goal of the proposed effort is to demonstrate feasibility of using selective laser melting (SLM, an emerging manufacturing technique) to manufacture a subscale combustion chamber liner that features an advanced regenerative cooling technique that combines high performance with low pressure drop. SLM enables the ability to "print" the advanced regenerative liner in mere hours, despite the liner's inherent flow passage complexity. This reduction in manufacturing lead time, combined with the fact that SLM manufacturing costs are driven almost exclusively by the amount of raw powder used during fabrication, results in a substantial cost reduction for future regeneratively-cooled rocket engines. Considering that the proposed regenerative cooling approach features heat transfer coefficients 3-10 times higher and pressure drops 2-10 times lower than traditional axial channels, the proposed effort demonstrate one of the highest performing, lowest cost combustion chambers in the world.

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

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