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Universal Docking Interface for Free-Flying Robots

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX17CA33P
Agency Tracking Number: 174380
Amount: $118,659.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: Z5.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2017
Award Year: 2017
Award Start Date (Proposal Award Date): 2017-06-09
Award End Date (Contract End Date): 2017-12-08
Small Business Information
63 Flushing Avenue Unit 150, Brooklyn, NY, 11205-1070
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jason Herman
 Director
 (646) 459-7819
 herman@honeybeerobotics.com
Business Contact
 Jason Herman
Title: Director
Phone: (646) 459-7819
Email: herman@honeybeerobotics.com
Research Institution
N/A
Abstract
Currently, no universal electromechanical engagement interface exists for free-flying robots, limiting their ability to dock, perch, recharge, change tools, manipulate payloads, and assemble in modular structures for intravehicular, extravehicular, and planetary surface operations. Honeybee Robotics (Honeybee) proposes to develop a Universal Docking Interface (UDI) that provides a common electromechanical connection architecture for free-flying robots. The UDI will enhance capabilities to mount and manipulate tools, sensors, payloads; dock for power and data transfer; perch for short- or long-term storage; and create new modular structures for intravehicular, extravehicular, and surface tasks in support of commercial operations and human spaceflight. The UDI will be based on Honeybee's existing solutions for robotic satellite servicing and planetary rover recharge , modified to meet NASA's Space Technology Mission Directorate (STMD) Human Exploration Telerobotics requirements. This reliable plug-and-play docking and manipulation interface will provide an electromechanical quick-connect/disconnect for tools, sensors, and other payloads, as well as enabling truly modular assembly in microgravity. The proposed Phase 1 effort will perform a detailed investigation of tool change, sensor payload interface, manipulation and docking requirements for free-flying robots supporting missions on-orbit, to Mars, the Moon, or NEOs. Interface requirements such as mate/de-mate cycles, stiffness, strength, repeatability, misalignment tolerance, human safety, debris mitigation, and electrical feedthrough characteristics will be derived through contact with potential end users to characterize potential use cases and future mission payloads.

* Information listed above is at the time of submission. *

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