Cyclops Hardware Validation Demonstration (Cyclops Demo) - 09.04.14

Overview | Description | Applications | Operations | Results | Publications | Imagery
ISS Science for Everyone

Science Objectives for Everyone
Launching satellites from Earth using rockets is expensive and risky, but small satellites can be delivered to the International Space Station (ISS) in larger groups, and then individually deployed from there. The Cyclops, also known as the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), ejects nanosatellites from  outside the ISS.  Nanosatelittes are inserted into the Cyclops platform inside the Japanese Experiment Module airlock then get moved to the outside of the ISS by the station’s robotic arms where they are deployed.

Science Results for Everyone
Information Pending



The following content was provided by Daniel R. Newswander, and is maintained in a database by the ISS Program Science Office.

Experiment Details

OpNom Cyclops

Principal Investigator(s)

  • Daniel R. Newswander, Houston, TX, United States

  • Co-Investigator(s)/Collaborator(s)
    Information Pending
    Developer(s)
    Johnson Space Center, Houston, TX, United States

    Sponsoring Space Agency
    National Aeronautics and Space Administration (NASA)

    Sponsoring Organization
    Technology Demonstration Office (TDO)

    Research Benefits
    Information Pending

    ISS Expedition Duration
    September 2014 - March 2015

    Expeditions Assigned
    41/42

    Previous ISS Missions
    Information Pending

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    Experiment Description

    Research Overview

    • Cyclops robotically deploys satellites from ISS, and is designed to provide the ISS Program with a method to transfer internally stowed satellites to the external environment. Cyclops’ mechanical interfaces are to the existing slide table located in the Japanese Experiment Module Pressurized Module (JEM PM) Airlock, and to the existing Special Purpose Dexterous Manipulator (SPDM) attached to the Space Station Remote Manipulator System (SSRMS) or the JEM Small Fine Arm (SFA).
    • Cyclops consists of the following major components:  deployment table with an internal capture and release mechanism, pusher plate mechanism to eject a satellite away from ISS, a grapple fixture interface to robotic utilities, a cone receptacle that interfaces to the JEM PM Slide Table, and passive retention hooks. A stowage container will also be developed but, for the purpose of this requirements document, is not considered to be part of the Cyclops.
    • The Cyclops is designed to provide a common payload interface and to accommodate payloads up to the internal volume of the JEM Airlock Slide Table.

    Description

    Cyclops is a mechanism used to robotically deploy satellites from ISS and is designed to provide the ISS Program with a method to transfer internally stowed satellites to the external environment. Cyclops mechanical interfaces are to the existing slide table located in the JEM PM Airlock and to the existing SPDM attached to the SSRMS and/or the JEM SFA. The Cyclops is designed to provide a common payload interface and to accommodate payloads up to the internal volume of the JEM Airlock Slide Table.

     

    Cyclops consists of the following major components:  deployment table with an internal capture and release mechanism, pusher plate mechanism to eject a satellite away from ISS, a grapple fixture interface to robotic utilities, a cone receptacle that interfaces to the JEM Air Lock Slide Table, and passive retention hooks. Cyclops fills the payload deployment gap between small cubesat launchers and major payloads enabling a whole new range of payload possibilities.


     

     

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    Applications

    Space Applications

    Cyclops enables the space-based launch of a new class of satellites, which are larger than cubesats but not large enough to require their own Earth-based launch vehicles. The facility's components include an internal capture-and-release mechanism, a pusher to eject a small satellite away from the space station, and a grappling fixture that connects to space station robotic tools. The Cyclops Demo investigation advances nano-satellite design, development and operation by testing the deployment of small satellites, including a nested satellite pair called Lonestar (University of Texas and Texas A&M University Collaboration) and a propulsion experiment called SpinSat (Department of Defense Space Test Program).

    Earth Applications

    Payloads launched on Cyclops vary in their research goals but often have educational or earth observation value.

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    Operations

    Operational Requirements
    Information Pending

    Operational Protocols

    • Crewmember attaches Cyclops to JEM Airlock Slide Table via clamping slide table mechanism.
    • Cyclops exits the ISS via the JEM Airlock, and interfaces with one of the robotic arms for deployment of attached payload.
     

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    Results/More Information

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    Related Websites

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    Imagery

    image
    Cyclops Image courtesy of NASA Johnson Space Center, Houston, TX

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    Cyclops Image courtesy of NASA Johnson Space Center, Houston, TX

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