|
The Global Leader of Portable Data Acquisition Solutions
|
|
1-888-714-3272 |
IOtech Events |
| Selection Guides | OEM Zone |
Solid-Propellant Missile Testing Used in a variety of applications, satellites house an array of expensive and highly sensitive equipment. Missiles and other high-altitude vehicles are used to launch these satellites into the Earths orbit. In some instances, harsh flight conditions put damaging stress on vital satellite instrumentation. Using a portable PC-based data acquisition system, engineers are able to monitor the effects of ambient factors during missile-test launches into orbit. Application Summary To evaluate how the TOMS satellite would be affected during launch, engineers needed to measure several variables in the carrier missiles fairing environment during flight. Variables included acoustic vibration, temperature, contamination, air velocity, humidity, heat transfer rate, and calorimeter voltage. Potential Solution IOtechs Solution The system featured IOtechs DaqBook, a portable PC-based data acquisition system. Housed in DBK10 expansion-card enclosures, the system featured three IOtech DBK expansion/signal conditioning cards. IOtechs DBK15 universal current/voltage card collected air velocity and pressure measurements. A DBK16 strain-gage card gathered data from two calorimeters, and four DBK82 high-accuracy thermocouple cards collected data from numerous sensors. A DBK30A battery module supplied power to all of the systems components. Mixed-analog signals were supplied by calorimeters, pressure transducers, humidity sensors, and air velocity sensors. The systems 256-channel capacity easily handled the tests 69-channel requirement. The DaqBooks 16-bit A/D resolution easily provided the required accuracy for the project. Software was used to control and view data as it was being collected, and LabVIEW® was used to analyze and present analog data after it was acquired. The software ran on an IOtech-recommended notebook PC that was seamlessly compatible with the system. Key to the projects success was the systems mobility and durability. The DaqBook and expansion modules matched the notebook PCs form factor (8.5 x 11.5 x 1.375) and were mounted on top of each other with brackets, creating a compact system that easily fit inside the payload assembly box. The total system weighed a total of 27.9 lbs., easily meeting the projects weight limitations. The DaqBook system easily withstood the harsh flight environments, thanks in part to its rugged metal enclosures that protected and isolated the systems circuitry. Conclusion |