Space Acceleration Measurement System-II (SAMS-II) - 11.18.15
Space Acceleration Measurement System-II (SAMS-II) is an ongoing study of the small forces (vibrations and accelerations) on the International Space Station (ISS) resulting from the operation of hardware, crew activities, dockings and maneuvering. Results generalize the types of vibrations affecting vibration-sensitive experiments. Investigators seek to better understand the vibration environment on the ISS. Science Results for Everyone Shaken, not stirred. That’s what happens to scientific experiments onboard the International Space Station (ISS), thanks to small forces created by vehicle and crew activities and by other experiments. Researchers used sensors to collect data on disturbances in the frequency range of 0.01 - 400 Hz and downlinked it to Glenn Research Center. Analysis of nearly 3.4 terabytes of data indicate that ISS is not meeting its goal of providing a quiescent, low-gravity environment for scientific research. Data also indicate that there is no clear reduction in disturbances during crew sleep periods. The measuring continues on an as-needed basis and data are available to the scientific community. Facility Details
OpNom: SAMS II
William Foster, Glenn Research Center, Cleveland, OH, United States
ZIN Technologies Incorporated, Cleveland, OH, United States
Sponsoring Space Agency
National Aeronautics and Space Administration (NASA)
Human Exploration and Operations Mission Directorate (HEOMD)
ISS Expedition Duration
March 2001 - December 2002; November 2002 - May 2003; April 2003 - September 2012; September 2013 - March 2016
Previous ISS Missions
SAMS, the precursor to SAMS-II flew on numerous shuttle flights since STS-40, including STS-107 (Columbia) which was lost in 2003. SAMS-II has been operating on ISS since Expedition 2.
- Space Acceleration Measurement System-II (SAMS-II) measures accelerations caused by vehicle, crew and equipment disturbances. These vibratory/transient accelerations occur in the frequency range 0.01 to 300 Hertz.
- Vibrations exist on the space station for a variety of reasons: equipment operation, structural motion, crew movement, and thermal expansion are but a few.
- Multiple sensors measure accelerations electromechanically at various locations in the US Lab.
- SAMS-II measurements help investigators characterize accelerations that influence International Space Station (ISS) experiments. The acceleration data is available to researchers via the World Wide Web.
Space Acceleration Measurement System-II (SAMS-II) measures vibrations from vehicle acceleration, systems operations, crew movements, and thermal expansion and contraction. Multiple Remote Triaxial Sensor (RTS) systems directly monitor individual experiments. Each RTS is capable of measuring between 0.01 Hz to beyond 300 Hz of vibration, also known as g-jitter. The RTSs consist of two components: the RTS sensor enclosure (SE) and the RTS electronics enclosure (EE). The RTS-SE, placed as close to the experiment as possible, translates the g-jitter into a digital signal. The RTS-EEs provide power and command signals for up to 2 RTS-SEs and receive the g-jitter data from the RTS-SEs. The RTSs are linked together by the Interim Control Unit (ICU), which coordinates the various RTS systems being used throughout the station. Eventually, the ICU will be replaced by a full-fledged Control Unit (CU), which will allow on board data analysis and direct feedback and will permit crew to control the measurement parameters. The main component of the ICU is a computer. Once the ICU receives the measurements from the RTS systems, it checks the data for completeness, and then sends the data to the SAMS-II Ground Operations Equipment in the TeleScience Center at Glenn Research Center in Cleveland, OH.
The SAMS-II RTS is installed in Rack 1, drawers 1 and 2, away from the Active Rack Isolation System (ARIS) in Rack 2, which could cause disruptions to measurements. The ICU is in Rack 2, drawer 1 prior to Increment 3. At the end of Increment 3, the crew transfers it to EXPRESS Rack 4. Once installed and activated, SAMS-II operates automatically.
SAMS-II measures subtle vibrations that affect only certain types of experiments and is not operational all the time. SAMS-II operates from the Glenn Research Center Telescience Support Center as needed. The ICU laptop has the capacity to save up to ten hours of data from five sensors working at maximum frequency range. This capacity is intended to act as a backup if downlink services are interrupted.
SAMS-II provides environmental data for scientific experiments that are conducted on board the ISS. Any degree of acceleration disturbance can ruin their science. In fluid physics and crystal growth, SAMS-II detects the vibrational disturbances that cause the microstructures to form undefined and disfigured. The liquid - solid transition is difficult when the amount of disturbances is high.
The residual acceleration environment of an orbiting spacecraft in low earth orbit is a complex phenomenon. Many factors, such as experiment operation, life-support systems, crew activities, aerodynamic drag, gravity gradient, rotational effects and the vehicle structural resonance frequencies (structural modes) contribute to form the overall reduced gravity environment. Weightlessness is an ideal state, which cannot be achieved in practice because of the various sources of acceleration present in an orbiting spacecraft. SAMS-II records acceleration disturbances caused by the ISS, its crew, and equipment. A complete understanding of the vibration environment will help researchers develop methods to minimize disturbances. It also allows other principal investigators to design their payloads with the vibration environment in mind.^ back to top
- The equipment is powered on when specific disturbances need to be analyzed and is controlled from the ground.
- The crew installs and removes sensor heads and cables to payloads.
- Crew occasionally complete filter cleaning and change out.
Decadal Survey Recommendations
Information Pending^ back to top
One of the major goals of the ISS is to provide a quiescent low-gravity environment to perform fundamental scientific research. However, small disturbances aboard the ISS impact the overall environment in which experiments are being performed. Such small disturbances need to be measured in order to assess their potential impact on the experiments. The Space Acceleration Measurement System - II (SAMS-II) is used on board the ISS to do just that.
SAMS-II measures accelerations caused by vehicle, crew, and experiment disturbances. SAMS-II measures the vibratory/transient accelerations, which occur in the frequency range of 0.01 - 400 Hz. The sensors measure the accelerations electronically and transmit the data to the Interim Control Unit (ICU) located in the EXPRESS Rack drawer. Data is collected from all the sensors and downlinked to the TeleScience Center at Glenn Research Center. The acceleration data is processed and made available to the microgravity scientific community at Principal Investigator Microgravity Services.
SAMS-II measures vibratory acceleration disturbances in microgravity and non-microgravity modes of ISS operations. Current data indicate that ISS is not meeting its microgravity mode design requirement, and that there is no clear reduction in these disturbances during crew sleep periods (DeLombard et al. 2005).
SAMS-II has collected over 3.4 terabytes of acceleration data, much of which have been processed and analyzed to characterize the reduced gravity environment on board the ISS in order to help science teams understand the ISS environment. SAMS-II, began to have some computer difficulties at the beginning of Expedition 12 (October 2005); the harddrive was replaced at the end of Expedition 14 (April 2007) and SAMS-II functions nominally on an as-needed basis.
Jules K, Hrovat K, Kelly EM, McPherson K, Reckart T, Grodsinsky C. International Space Station Increment-3 Microgravity Environment Summary Report. NASA Technical Memorandum; 2002.
DeLombard R, Kelly EM, Jules K, Hrovat K, McPherson K. An Overview of the Microgravity Environment of the International Space Station Under Construction. 40th Aerospace Sciences Meeting and Exhibit, Reno, NV; 2002
Jules K, Hrovat K, Kelly EM, Reckart T. International Space Station Increment 6/8 Microgravity Environment Summary Report November 2002 to April 2004. NASA Technical Memorandum; 2006.
Jules K, McPherson A, Hrovat K, Kelly EM. Initial Characterization of the Microgravity Environment of the International Space Station: Increments 2 Through 4. Acta Astronautica. 2004 Nov; 55(10): 855-887.
DeLombard R, Hrovat K, Kelly EM, McPherson K. Microgravity Environment on the International Space Station. 42nd Aerospace Sciences Meeting and Exhibit, Reno, NV; 2004
Jules K, McPherson K, Hrovat K, Kelly EM, Reckart T. International Space Station Increment-2 Microgravity Environment Summary Report. NASA Technical Memorandum; 2002.
Saez N, Ruiz X, Gavalda F, Shevtsova V. Comparative analyses of ESA, NASA and JAXA signals of acceleration during the SODI-IVIDIL experiment. Microgravity Science and Technology. 2014 July; 26(1): 57-64. DOI: 10.1007/s12217-014-9376-y.
McPherson K, Kelly EM, Keller J, Goto M. Acceleration Measurement Opportunities on the International Space Station. 59th International Astronautical Congress. Glasgow, Scotland; 2008
Jules K, Hrovat K, Kelly EM. International Space Station Increment-2 Quick Look Report. NASA Technical Memorandum; 2002.
Zavalishin DA, Belyaev MY, Sazonov VV. Study of vibration microaccelerations onboard the International Space Station. Cosmic Research. 2013 July 19; 51(4): 261-269. DOI: 10.1134/S0010952513040096. [Original Russian Text © D.A. Zavalishin, M.Yu. Belyaev, V.V. Sazonov, 2013, published in Kosmicheskie Issledovaniya, 2013, Vol. 51, No. 4, pp. 294–302.]
McPherson K, Kelly EM, Keller J. Acceleration environment of the ISS. 47th Aerospace Sciences Meeting and Exhibit, Orlando, FL; 2009
DeLombard R, Hrovat K, Kelly EM, Humphreys BT. Interpreting the International Space Station Microgravity Environment. 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV; 2005
Ground Based Results Publications
DeLombard R. Disturbance of the microgravity environment by experiments. AIP Conference Proceedings: Space Technology and Applications International Forum, Albuquerque, NM; 2000 614-618.
- Space Acceleration Measurements System - II
- Principal Investigator Microgravity Services
- SpaceRef.com - End of an Era for SAMS
NASA Image: ISS004E8406 - SAMS sensor head mounted near top of EXPRESS Rack 2 in U.S. Lab taken during Expedition 4.
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NASA Image: ISS008E11936 - SAMS-II in EXPRESS Rack 4 in U.S. Lab during Expedition 8.
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NASA Image: ISS007E06980 - Back-dropped by the blackness of space and Earth's horizon, an unmanned Progress supply vehicle approaches the ISS during Expedition 7. Inset image shows microgravity acceleration data provided by the SAMS-II hardware during a Progress docking with ISS.
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NASA Image: ISS027E009634 - Documentation of a Space Acceleration Measurement System (SAMS) sensor installed at location LAB1S1 in the Destiny U.S. Laboratory during Expedition 27.
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