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Acceleration Measurement Program (AMP)

Managed By: NASA

Implementation Partner: ZIN Technologies

Hardware Details

Specifications:
Space Acceleration Measurement System (SAMS):

  • measure local vibratory regime in all 3 of the ISS labs, including throughout the USL ( 0.01 ≤ f ≤ 300 Hz ).
  • SAMS sensor are deployed in all 3 laboratories
  • Two SAMS RTS drawers (original SAMS technology, flight 6A)
  • Each drawer consists of an Electronics Enclosure (EE) and connectivity for two Sensor Enclosures (SE)
  • RTS drawers located in EXPRESS Rack #1 (LAB1O2) and EXPRESS Rack #4 (JEM1F5)
  • ARIS Equipped EXPRESS racks are equipped with an embedded Electronics Enclosure
  • EXPRESS Rack #2 (LAB1O1) and EXPRESS Rack #3 (COL1A1) are currently used by SAMS
  • EXPRESS Rack #7 (LAB1P2) and EXPRESS Rack #8 (LAB1P4) are available for use by SAMS
  • SAMS TSH-ES (Triaxial Sensor Head – Ethernet Standalone)
  • New SAMS sensor technology dedicated to the FIR, CIR, and MSG facilities
  • No Electronics Enclosure (EE) required
  • SAMS Seat Track Device (STD) used for mounting SAMS SE sensors in “unplanned” locations using the rack seat track design
  • Two units available currently

Microgravity Acceleration Measurement System (MAMS)

  • measures the quasi-steady acceleration regime ( f < 0.01 Hz )
  • data can be mapped to any location (rigid-body assumed)

Related Documents

http://www.spacestationresearch.com/wp-content/uploads/ZIN-AMP-Summary.pdf

Related Links

https://spaceflightsystems.grc.nasa.gov/sopo/ihho/psrp/acceleration/ https://spaceflightsystems.grc.nasa.gov/sopo/ihho/psrp/acceleration/mams/ https://spaceflightsystems.grc.nasa.gov/sopo/ihho/psrp/acceleration/sams/

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