Elastic Memory Composite Hinge (EMCH) will study the performance of a new type of composite hinge to determine its suitability for use in space. The experiment uses elastic memory hinges to move an attached mass at one end. Materials tested in this experiment are stronger and lighter than current materials used in space hinges and could be used in the design of future spacecraft.Principal Investigator(s)
United States Department of Defense Space Test Program, Johnson Space Center, Houston, TX, United States
Composite Technology Development, Incorporated, Lafayette, CO, United States
National Aeronautics and Space Administration (NASA)Sponsoring Organization
Department of Defense (DoD) - RetiredResearch Benefits
Information PendingISS Expedition Duration
April 2007 - October 2007Expeditions Assigned
15Previous ISS Missions
The Lightweight Flexible Solar Array Hinge - LFSAH, a precursor to EMCH was flown on STS-93.
The Elastic Memory Composite Hinge (EMCH) experiment provided test data on new materials that will further
space hardware technology. This technology may eliminate the need for highly complex deployment mechanisms by
providing a simpler, lightweight alternative to mechanical hinges. EMCH builds on the previous Space Shuttle
experiment, Lightweight Flexible Solar Array Hinge (LFSAH) flown on STS-93.
The six EMCH test articles tested on the International Space Station (ISS) were approximately 10 x 2.5 x 2.5 cm in dimension and made of a unique resin and carbon fiber laminate developed at Composite Technology Development, Inc. End fixtures and metrology devices were developed to allow the EMCH test articles to be deployed through remote actuation, while their force-torque history and deployment accuracy are recorded automatically. A resistive heater was embedded in the Elastic Memory Composite (EMC) laminates in the hinge to provide the heat necessary for actuation. The hinge was folded on the ground and deployed in space. A proximity sensor was attached to the end mass to determine the final position upon deployment. A second motion sensor was used to determine the deployment versus time history. The test articles were re-settable to allow for multiple deployments.
EMC materials tested in this experiment are stronger and lighter than current material used in space hinges and could be used in the design of future spacecraft.Earth Applications
Since composite materials are valued for being lightweight and strong, the hinges may have spin-off applications on Earth.
The crewmember applies power to the experiment, waits for the hinges to reach the appropriate temperature, and then proceeds to activate each hinge individually. Video and photo documentation of deployments is required. Reheating of the test articles will allow the crewmember to return the hinges to their stowed position using the control panel on the EMCH chassis. A full cycle (power on, hinge deployment, hinge reset) will be less than 90 Minutes. Once the hinges have been reset, deployments can be activated again. Data downlink of hinge deployments is required.Operational Protocols
EMCH will be launched in a bag on the 12A.1. It will be transitioned to ISS and stored in a locker. During use, it will be attached to the outside of the ISS rack then returned. Photo and video will be required.
EMCH was successfully completed onboard the ISS during Expedition 15. The investigation was returned to Earth for a complete analysis by the investigator team in 2007. However, the preliminary assessment indicated that the experiment demonstrated the robustness and reliability of the TEMBOŽ EMC hinge in the zero-gravity environment. This test campaign consisted of both nominal and off-nominal conditions, with the final series of tests presenting the most challenging conditions for on-orbit TEMBOŽ hinges. The successful completion of these tests indicate that hinges meet the designed performance goals of a next-generation spaceflight-qualified actuator. Additionally, the science gained from this experiment confirms engineering assumptions used to design the TEMBOŽ EMC hinges, as well as other TEMBOŽ EMC deployable structures that are being developed for space applications. (Evans et al. 2009)
Barret R, Francis W, Abrahamson E, Lake M. Qualification of Elastic Memory Composite Hinges for Spaceflight Application. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, RI; 2006 May 2006-2039.