NASA STTR 2020-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 20-1- T12.01-4984
SUBTOPIC TITLE:
 Thin-Ply Composite Technology and Applications
PROPOSAL TITLE:
 Creep-Resistant Aromatic Polyester Thermosets for Thin-Ply Composites
SMALL BUSINESS CONCERN (SBC):
ATSP Innovations
60 Hazelwood Drive
Champaign IL  61820 - 7460
Phone: (217) 778-4400
RESEARCH INSTITUTION (RI):
Texas A&M Engineering Experiment Station
400 Harvey Mitchell Parkway South
TX  77845 - 3578
Phone: (979) 458-2556

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Jacob Meyer
E-mail:
jacob.l.meyer@atspinnovations.com
Address:
60 Hazelwood Drive Champaign, IL 61820 - 7460
Phone:
(217) 778-4400

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Jacob Meyer
E-mail:
jacob.l.meyer@atspinnovations.com
Address:
60 Hazelwood Drive Champaign, IL 61820 - 7460
Phone:
(217) 778-4400
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words)

For deployment of future space structures, volume-minimized methods of rolling/folding carbon fiber composites during launch may be attractive. Due to the high strain and potential elevated temperatures during launch, there is concern about creep and therefore distortion of the composite member. ATSP Innovations and team partner Texas A&M University propose a unique thin ply composite for inflatable and rollable/foldable space structure concepts. ATSP Innovations has developed a new family of high performance resins called Aromatic ThermoSetting coPolyesters, which have Tg ranging from 174-310C and high thermal stability. In Phase I, we seek to produce a modified resin system with a lower temperature cure profile and fabricate this resin into thin-ply ATSP-carbon fiber reinforced composites. Initially, a matrix of formulated resins and catalyst concentrations will be synthesized and examined in terms of themomechanical properties. ATSP and Texas A&M will characterize and model the resins creep and stress relaxation properties. The best performing resin in terms of thermomechanical properties, viscosity, and cure profile will be selected for prepregging into thin-ply composites and cured into coupons for further creep and stress relaxation experiments. A film adhesive interlayer useful for production of the desired thin-walled members will also be developed and initially demonstrated. A nonlinear thermo-viscoelastic constitutive model will be formulated for the general anisotropic material as determined from experiments. This will be coupled with a microstructural model and structural model to predict behavior of thin-ply composite. In Phase II, ATSP Innovations will also investigate appropriate fabrication methods for producing rollable composite members as well as key metrics for their viability in space applications. 

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

Rollable/foldable composites with creep and environmental resistance and modest processing requirements would be attactive as a method for minimizing mass and volume for deploying large area space structures relevant for next-generation observatories. Specific examples may include composite booms, landing struts, space habitats, and other lightweight structures. As well, the developed creep-resistant thin-ply composite may impact designs in advanced aviation systems including supersonic and hypersonic technology development and launch systems. 

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

Thin-ply, creep resistant carbon-fiber composites with attractive cure profiles may be viable as a lightweighting concept in the automotive and aerospace markets. The developed resin system would also be attractive generally in most performance composite market spaces. Impact could extend into multiple areas such as microelectronics, tribological coatings, rigid structural foams, etc.

Duration: 13

Form Generated on 06/29/2020 21:13:43