SBIR/STTR Research Award

Modeling Nonlinear Viscoelasticity and Time-Dependent Yielding of Thin-Ply Composites

Award identifier 0d0fa0f153ccaeb8dab8f7951b583368556532a87a3288deac66ed8d6a737beeAwarding agency National Aeronautics and Space Administration

Award amount

$124,952

Program and phase

STTR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ANALYSWIFT, LLC
Proposal award date
2020-08-25
Contract end date
2021-09-30
UEI
CDJ1KMBUAFA4
Solicitation number
STTR_20_P1
Topic code
T12

Research abstract

This project aims at developing a modeling framework capable of accurately predicting the nonlinear viscoelastic and time-dependent yield behavior of thin-ply composite laminates for the reliable design of deployable spacecraft structures. For applications in deployable spacecraft structures, thin-ply composites are currently made from spread-tow carbon fabrics impregnated with epoxy polymer matrices. The polymer matrix exhibits a strongly time-dependent mechanical response, which means that its current stress or strain state is influenced by the loading and temperature histories. Polymers go through several distinct regimes of behavior as the strain level increases, which are characterized by linear viscoelasticity, nonlinear viscoelasticity, time-dependent yielding, viscoplasticity, and time-dependent fracture. A complete constitutive description of all these deformation stages, and incorporation of these behaviors in thin-ply composite laminates, is highly challenging and requires a multi-year effort, but is critical because composite deployable structures are folded to high curvatures for extended periods of time. Previous experiments have shown that an extended stowage time can lead to incomplete deployment, like in the case of the MARSIS instrument in the Mars Express Orbiter mission, and partially recovered deployed shape, resulting in low performance and reliability.nbsp;The proposed effort is a step towards meeting this challenge by focusing on modeling the nonlinear viscoelastic response that precedes permanent deformation as well as the time-dependent yield limits of thin-ply composites. The underlying computational framework is based on the mechanics of structure genome (MSG) [ref msg paper], a recently discovered unified approach for multiscale constitutive modeling of composite structures, and formulated with finite kinematic measures. The material constitutive models are physics-based and informed by appropriate experiments.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

12 SBIR/STTR records share this UEI (2019–2026). Reported award amounts total $2,445,768. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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