SBIR/STTR Research Award

Reversible Adhesion Concept for In-Space Assembly

Award identifier 32f0e2eafe836543eaa69e9aaf1b8804519c5a3c1a9e35fdc03b7beb73764a08Awarding agency National Aeronautics and Space Administration

Award amount

$749,992

Program and phase

SBIR · Phase II

Award year

2018

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ATSP Innovations, Inc.
Proposal award date
2018-04-26
Contract end date
2020-04-25
UEI
D1E4E2QKPKR4
Solicitation number
SBIR_17_P2
Topic code
Z4

Research abstract

ATSP Innovations will develop a reversible adhesion concept for use in reconfigurable space frame construction. This reversible adhesion concept is based on application of aromatic thermosetting copolyester (ATSP) to selected adhesive contact points. By virtue of a class of reversible solid-state chemical reactions (called interchain transesterification reactions - ITR) intrinsic to the polymer, ATSP was shown to bond and debond with itself for >50 cycles during the Phase I with high mechanical strength allowing load values >6 the requirement of the solicitation in an very small contact area.In Phase II of this project we will apply this reversible adhesive concept to assembly and reconfiguration of truss structures composed of tubular beams and we will do electrical, thermal and mechanical characterizations of the reversibly joined tube segments. Based on the reversible adhesion concept developed and demonstrated in Phase I, a self-aligning attachment mechanism for tubular beams and hub joints with integrated heating is proposed. Designed attachment mechanisms and developed processes will be applied to assembly and reconfiguration of truss unit cell. Polymeric reversible adhesive will be subjected to outgassing and radiation experiments (to determine applicability to space environment) in simulation of low earth orbit with additional bond/debond cycles following radiation exposure implemented via a toolkit developed in Phase I. The high mechanical strength provides design flexibility for space in the joints for electrical contacts, thereby allowing multifunctionality of the space structures; with full scale dimension of the real truss structure, the joint would be able to reach a bond strength of 56,760N (113 times the required500N).

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.

Research funding history

21 SBIR/STTR records share this UEI (2011–2025). Reported award amounts total $8,698,427. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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