National Aeronautics and Space Administration National Aeronautics and Space Administration The U.S. Government's Official Web Portal National Aeronautics and Space Administration National Aeronautics and Space Administration
NASA Banner spacer Banner Spacer spacer spacer
Advanced Search
Go button
spacer About NASA About NASA Glenn Exploration Systems Mission Directorate
Space Flight Systems @ GRC SAMS banner
News & Events
Orion Project Office
Launch Systems Project Office
Constellation Office
Announcement Background spacer
Advanced Flight Projects Office
Space Acceleration Measurements System II (SAMS-II)


SAMS Status

August 21, 2009 - The SAMS acceleration system on board the International Space Station is supporting the international partners by relocating existing SAMS sensors to different ISS modules.  SAMS provided acceleration data to the JAXA researchers during May 2009 for the experiments located in the Japanese Experiment Module (JEM). SAMS also provided a sensor and acceleration data for the European Space Agency (ESA) in the Columbus Orbital Facility (COF) during March of 2009.

SAMS is a distributed system of sensors, currently on board the ISS, SAMS has two sensors located in the USLab, two sensors in the JEM,  one sensor in the COF, one sensor attached to the CIR, and one sensor in the MSG facility.

Overview

SAMS-II will measure vibrations from vehicle acceleration, systems operations, crew movements, and thermal expansion and contraction. Multiple Remote Triaxial Sensor (RTS) systems are used to monitor individual experiments requiring direct monitoring. 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, will translate the g-jitter into a digital signal. The RTS-EEs provides power and command signals for up to 2 RTS-SEs and receives 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 onboard 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 the computer sends the data to the SAMS-II Ground Operations Equipment at Glenn Research Center.

Related Web Sites

* Principal Investigator Microgravity Services (PIMS) Results Home Page
* NASA Glenn Research Center - SAMS
* NASA Glenn Research Center - MAMS

 


 

 


Contacts at NASA Glenn Research Center
Project Manager: Robert W. Hawersaat

Robert.W.Hawersaat@nasa.gov
216-433-8157


ISS Research Program
Fluids & Combustion Facility
FCF Investigations
Microgravity Science Glovebox
Acceleration Measurements
MAMS
SAMS
PIMS
Maintenance Work Area
Expendable Launch Vehicle Investigations
Telescience Support Center
Human Research Program
Science Project Office
Advanced Capabilities Project Office
Space Operations Project Office
National Center for Space Exploration Research
External Partners
Education/Outreach
Space Exploration Benefits
Program Support
 
Acceleration Links
pdf icon Publications & Presentations
   
   
Space Flight Systems Links
Acronyms  
Articles
 
Missions  
Site Map
 
This Month in Exploration  
   
   
GRC Microgravity and Technology Flight Experiments
Accomplished  
Planned  
   
   
Acceleration Related Documents
small acrobat icon  SAMS Overview Chart  
   
small acrobat icon  MAMS Overview Chart  
   
small acrobat icon  PIMS Overview Chart  
Footer seperator
FirstGov Logo

+ Freedom of Information Act
+ Privacy Policy and Important Notices
+ Applications and Plugins for Viewing Documents and Media
NASA Logo

Webmaster:
Tim Reckart
NASA Official: Thomas St. Onge
Last Updated: October 7, 2009
Footer spacer
Footer spacer