Invocon on the International Space Station
Currently, Invocon has three systems in operation on the International Space Station (ISS): Internal Wireless Instrumentation System (IWIS™),External Wireless Instrumentation System (EWIS™), and Micro-gravity Measurement Apparatus (MMA).
IWIS was deployed by astronauts inside the partially completed ISS to collect
data on the impulse response of the structure.
This data is used to verify the structural integrity of the ISS on orbit.
It
will also be used to update models predicting the modal response of the ISS.
Complete understanding of the resonant modes of the structure will allow
effective planning of the re-boost and Reaction Control System (RCS) firing
sequences when the Shuttle is docked with the Station.
Since this data will change as the Station is assembled, it is important to keep
this data current with each addition to the Station.
The wireless nature of the data acquisition network minimizes the time necessary
for deployment and recovery of the system.
Further, some of the RCS test firings must occur when all airlocks between
modules are closed. A wired system
would not have the flexibility needed to accommodate mission changes and data
acquisition windows of opportunity.
The first element of EWIS was deployed by the STS-115 crew as part of the installation of the P3/P4 truss. EWIS was developed as a system for acquiring vibration data from the truss structure to monitor the health of the truss components. The single EWIS Remote Sensor Unit (RSU) attached to the truss is currently collecting vibration data. This vibration data will be downloaded when the EWIS Network Control Unit (NCU) is installed during a future mission.
Click here for more information about the Wireless Instrumentation System (WIS™) family
In
2008 the Japan Aerospace Exploration Agency (JAXA) will launch a module
for the ISS that will contain another permanent Invocon system:
Micro-gravity Measurement Apparatus (MMA). This system is designed to
constantly monitor micro-vibrations in the Station that could adversely affect
zero-g experiments. MMA Qual hardware was delivered in September, 2002.
Flight Hardware is scheduled for delivery the first quarter of 2003.
Click here for more information about the Micro-gravity Measurement Apparatus (MMA)