NASA SBIR 2018-I Solicitation

Proposal Summary

 18-1- Z4.02-4552
 In-Space Sub-Modular Assembly
 Flexible Interconnecting NodEs for In-Space Structural Assembly (FINESS)
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
2602 Clover Basin Drive, Suite D
Longmont , CO 80503-7555
(303) 200-0068

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Kevin Cox
2602 Clover Basin Drive, Suite D Longmont, CO 80503 - 7555
(303) 263-8575

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Stephanie Amend
2602 Clover Basin Drive, Suite D Longmont, CO 80503 - 7555
(300) 200-0068
Estimated Technology Readiness Level (TRL) :
Begin: 3
End: 4
Technical Abstract

In response to NASA’s need for long-duration, low-mass in-space modular construction components, Roccor proposes to develop structural joints designed for rapid in-space assembly (iSA) and structural modularity. Trusses built of repeating unit-cell/modular elements can be assembled by connecting multiple modules to interconnecting joints.  Implemented with embedded conductors for connection verification, power and data transmission, the proposed invention utilizes near zero CTE composite tubes with snap-fit connectors and a flexible joint for quick, repeatable construction and reconfiguration of trusses in space.  The concenpt, Flexible Interconnecting NodEs for in-Space Structural Assembly (FINESS), will advance iSA opportunities through innovative features such as: 1) assembly connections at low-weight, low cost, and minimal part-count, 2) developing rigid plug-and-play joints for connecting modules in various arrangements, 3) integrating conductive elements for a fully connected structure with joint connection verification, and 4) near zero thermal expansion in carbon fiber tubes and connecting fixtures.  The principal objective for the Phase I project is to conduct a preliminary design-analysis-fabrication-test loop for an electrically integrated modular truss joint.  The project will clearly identify engineering risks that must be addressed to ensure acceptable performance on-orbit and in gravity loaded environments.  Detailed mechanical and electrical design will be performed including investigation of attainable truss geometries, repeatable plug-and-play fastening mechanisms, material selection and conductive routing.  The design efforts will be followed by local and global strength, stability and thermal analyses to describe the capacity of the modular joints.  Furthermore, elements of the concept will be prototyped to test areas such as modular assembly and electrical continuity across joints.

Potential NASA Applications

The FINESS system fills critical gaps in current capabilities and aligns perfectly with some of NASA’s recently established priorities: providing rapidly constructible structures implemented with electrical connectivity for routing power and data around joints, providing joint connection verification and providing a high degree of modularity at a small mass and stowage volume. The number of structural applications for the FINESS system really is endless due to its modular simplicity.

Potential Non-NASA Applications

In addition to NASA’s mission market, Roccor has identified other markets where advancements of the proposed FINESS system could have considerable impact: a) portable and man-packable constructible trusses for military ground troops, b) structural assemblies for lunar/Martian habitats and vehicles, c) rapid assembly of buoyancy devices in the absence of auto-inflation.

Form Generated on 05/25/2018 12:02:15