Optimal Composite Materials using NASA Resins or POSS Nanoparticle Modifications for Low Cost Fabrication of Large Composite Aerospace Structures

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$68,204.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
NNL05AA89P
Award Id:
76835
Agency Tracking Number:
041123
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
134 Sandy Drive, Newark, DE, 19713
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
960998474
Principal Investigator:
MarkGruber
Principal Investigator
(302) 369-5390
mgruber@accudyne.com
Business Contact:
MarkGruber
Business Official
(302) 369-5390
mgruber@accudyne.com
Research Institute:
n/a
Abstract
Reduced mass composite materials are crucial to the success of aerospace systems, but their adoption is inhibited because they require autoclave consolidation, a process that is prohibitively expensive for large aerospace structure. To remedy this, NASA-LaRC has been developing cost-effective high-performance thermoplastic composite processing equipment that enables out-of-autoclave tape placement. In particular, NASA is working with Accudyne Systems to install a heated in situ deposition placement head to fit on NASA-LaRC's placement machine. This SBIR is to create the optimal composite material feedstock to go hand-in-hand with the thermoplastic process equipment so as to create desirable mechanical and physical properties in a part with out-of-autoclave in-situ placement. Accudyne Systems will define the matrix resin and fabricate thermoplastic tape to create the ideal in situ processible material. The first approach will be to proveout a fully amorphous composite based upon NASA 8515. This avoids the undesirable kinetics of a semi-crystalline thermoplastic like PEEK. The second approach will be to use POSS nanoparticles in semi-crystalline PEEK to accelerate crystallinity to the short time scale of the in situ process.The best options will be commercialized to allow NASA and aerospace primes to fabricate low-cost large composite structure for air and space transport.

* information listed above is at the time of submission.

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