Skip to content

Textile Strain Measurement System

Miniature data recorder with resistive sensor input and built-in 3-axis accelerometer.

AIAA PUBLICATIONS

Textile Strain Measurement System
17-21 June 2019 | AIAA Aviation 2019 Forum

Textile Strain Measurement System Progress Update and Production Versions
16-19 May 2022 | 26th AIAA Aerodynamic Decelerator Systems Technology Conference

The Textile Strain Measurement System (TSMS) recorder is compact, self-contained data acquisition equipment developed under a NASA SBIR and built for the tough conditions typical during parachute deployment and inflation. The built-in accelerometer and external sensor inputs extend the recorder’s versatility to any project to capture the necessary data.
Contact Us to discuss your project with TSMS.

Mechanical

Dimensions:
27.3 x 22 x 8.6 mm (L x W x H)

Mass:
8.2 grams

Connectors:
USB interface 7-position socket header, 2.54 mm pitch
Sensor input 2-position socket header, 5.08 mm pitch

Electrical

Power Supply:
3.7 volt rechargeable battery, 85 mAh, on-board switched
USB power regulated to 2.8 volts via adapter cable and interface board

Current Draw:
~0.9 mA standby
<10 mA recording

USB Charging:
3.7 volts rate-limited to 1/2C via adapter cable and interface board

Operational

Memory:
16,000 samples, non-volatile

Acceleration:
3-axis MEMS accelerometer
100, 200, 400 g range selectable
1, 5, 50, 100, 400, 1000 Hz sample rate selectable

Analog-to-Digital (ADC):
Wheatstone bridge configuration
0-100 Ω, 0-10 kΩ ranges selectable
5, 20, 45, 90, 175, 330, 660, 1000 Hz sample rate selectable

Environmental

Thermal: -20 to 60 °C (-4 to 140 °F)

Acceleration: 100 g minimum sustained, any axis

Altitude: 10,600 m (35,000 ft) minimum or ~240 mbar (3.5 psia) at -18° C (O° F)

 

ALD Systems