Cyclops (Cyclops) - 09.06.17

Summary | Overview | Operations | Results | Publications | Imagery

ISS Science for Everyone

Science Objectives for Everyone
The 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. The 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.
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.
Facility Details

OpNom: Cyclops

Facility Manager(s)
Robert Zurawski, Ph.D., Johnson Space Center, Houston, TX, United States

Facility Representative(s)
Information Pending

Developer(s)
NASA Johnson Space Center, Houston, TX, United States

Sponsoring Space Agency
National Aeronautics and Space Administration (NASA)

Sponsoring Organization
Technology Demonstration Office (TDO)

ISS Expedition Duration
March 2014 - March 2015

Expeditions Assigned
39/40,41/42

Previous Missions
Information Pending

Availability

  • Planned
  • ^ back to top

    Facility Description

    Facility Overview
    The 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. Cyclops fills the payload deployment gap between small cubesat launchers and major payloads enabling a whole new range of payload possibilities.

    ^ back to top

    Operations

    Facility Operations

    1. Crew attachesCyclopsto JEM Airlock Slide Table via clamping slide table mechanism.
    2. Crew attaches payload to Cyclops and sets pusher mechanism
    3. Cyclops and payload are processed through JEM Airlock
    4. Robotic Arm grapples Cyclops w/attached payload
    5. JEM Airlock slide table mechanism unclamps Cyclops w/attached payload
    6. Robotic Arm positions Cyclops w/attached payload to deployment position
    7. Robotic Arm actuates internal mechanisms for deployment
    8. Payload is deployed perpendicular to Cyclops
    9. Cyclops placed back inside ISS (and stowed for future deployments) via Robotic arm  and JEM Airlock

    ^ back to top

    Decadal Survey Recommendations

    Information Pending

    ^ back to top
    Results/More Information

    Information Pending

    Results Publications

    ^ back to top

    Ground Based Results Publications

    ^ back to top

    ISS Patents

    ^ back to top

    Related Publications

    ^ back to top

    Related Websites

    ^ back to top


    Imagery

    image
    NASA Image: ISS042E016845 - The Special Purpose Inexpensive Satellite (SpinSat) following its release from the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), or Cyclops, launch platform. Cyclops is grappled by the Japanese Experiment Module Remote Manipulator System (JEMRMS) Small Fine Arm (SFA).

    + View Larger Image


    image
    NASA Image: ISS042E015943 - Commander Barry Wilmore unpacks the Cyclops launch platform for installation on the Japanese Experiment Module Airlock (JEMAL) slide table. The Cyclops platform, also known as the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), holds and ejects nanosatellites from outside the International Space Station (ISS).

    + View Larger Image


    image
    NASA Image: ISS042E015971 - Commander Barry Wilmore and flight engineer Terry Virts are photographed during operations to install the Cyclops launch platform on the Japanese Experiment Module Airlock (JEMAL) slide table. The Cyclops platform, also known as the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), holds and ejects nanosatellites from outside the International Space Station (ISS).

    + View Larger Image


    image
    NASA Image: ISS042E016072 - Flight engineer Terry Virts uses a video camera to document the Special Purpose Inexpensive Satellite (SpinSat) and Cyclops Platform on the Japanese Experiment Module Airlock (JEMAL) slide table. The Cyclops platform, also known as the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), holds and ejects nanosatellites from outside the International Space Station (ISS). The objective of the SpinSat experiment is to fly a 22-inch diameter spherical satellite equipped with an array of electrically-controlled solid propellant thrusters.

    + View Larger Image


    image
    NASA Image: ISS042E016906 - The Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), or Cyclops, launch platform with Special Purpose Inexpensive Satellite (SpinSat) attached is grappled by the Japanese Experiment Module Remote Manipulator System (JEMRMS) Small Fine Arm (SFA) in preparation for the release of SpinSat.

    + View Larger Image


    image
    NASA Image: ISS042E016822 - The Special Purpose Inexpensive Satellite (SpinSat) following its release from the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), or Cyclops, launch platform. Cyclops is grappled by the Japanese Experiment Module Remote Manipulator System (JEMRMS) Small Fine Arm (SFA).

    + View Larger Image