IN RESPONSE TO NASA S NEED FOR LONG-DURATION, LOW-MASS IN-SPACE MODULAR CONSTRUCTION COMPONENTS, ROCCOR PRO…

Public award description

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 I NTERCONNECTING 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 PLUGAND- 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.