No-Oven, No-Autoclave, Composite Processing

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX11CE48P
Agency Tracking Number: 104076
Amount: $100,000.00
Phase: Phase I
Program: SBIR
Awards Year: 2011
Solicitation Year: 2010
Solicitation Topic Code: X5.03
Solicitation Number: N/A
Small Business Information
OH, Dayton, OH, 45440-3638
DUNS: 130020209
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Michael Rauscher
 Principal Investigator
 (937) 320-1877
 rauschermd@crgrp.com
Business Contact
 Stephen Vining
Title: Business Official
Phone: (937) 320-1877
Email: viningsd@crgrp.net
Research Institution
 Stub
Abstract
Large, single-piece composite structures for NASA launch vehicles are currently very expensive or impossible to fabricate partly because of the capital (ovens, autoclaves, and tooling) needed to cure the part and maintain tolerances at cure conditions. CRG proposes the use of recently developed, no-oven, no-autoclave composite processing technology to fabricate very large, high-performance, single-piece composite structures and tooling for NASA launch vehicles and other aerospace structures. This will reduce capital (plant, equipment, and tooling), operating, and labor-based manufacturing costs. This technology enables rapid manufacturing of large, single-piece structures with no dependence on size-limiting infrastructure and offers the potential for on-site manufacturing. CRG believes this technology to be equally beneficial for quick throughput in smaller sized, high-volume production; but the proposed focus will be large, low-volume production. This technology proposes to surpass current efforts on out-of-autoclave composite processing technology in terms of both acquisition and operations cost to the end user. This will be accomplished through lower production costs and lightweight, unitized structures that require less maintenance. This three-phase program proposes to advance this technology from a Technology Readiness Level (TRL) of 4 and a Manufacturing Readiness Level (MRL) of 3 to a TRL of 9 and a MRL of 9.

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

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