World Wide Web — A new development in rocketry electronics is the rocket data-acquisition system developed by Advanced Electronic Devices of the Netherlands.

This system is used for measuring and storing analog and digital data gathered during the rocket flight as well as can be used to set off your pilot and main parachute charges.

The R-DAS system pictured here was developed by AED with the many lessons they learned from launching amateur rockets in mind.

The whole system is built on a very compact double-sided printed circuit board -- small enough to fit in almost any high-power or amateur rocket.

The picture shows a prototype, which is currently undergoing final testing.

The unit is configured with Windows software (Image 1, Image 2), allowing control of either a G-switch and/or breaking wire arming, smart recovery (integrating accelerometer, barometric main parachute) and/or timed recovery, barometric altitude for main chute release, extra data-acquisition channels, and sampling rate. It has a rather large amount of data storage to allow ambient pressure and acceleration to be sampled 250 times per second for more than 6 minutes. At lower sampling rates the sampling time is proportionally longer.

The large RAM memory of R-DAS is continuously updated with the last 10 seconds of pre-flight data. After lift-off the unit starts storing the data in EEPROM, starting with the last 10 seconds before lift-off. In this manner, pre-flight data is also available, e.g. for offset calibration, or drift verification. Six analog input channels are available through a 16-pin boxed header for your own experiments. This connector also provides your experimental board with a 9V power supply. Four digital inputs/outputs allow you to start your experiment at a pre-programmed time, switch on a recovery transmitter, or read the status from a a digital indicator.

And, R-DAS is available now! The production version R-DAS has the following extra features:

• Smaller unit, due to more extensive use of SMD components
• Professional 2-layer PCB
• User selectable high power output stages with continuity check. User selects 1A current source for reliable Davey Fire ignition, or maximum current output (limited by batteries)
• Extra battery connection for ignitor output stages
• ADXL50 accelerometer will be replaced with the new ADXL150 transducer (less noise, higher bandwidth)
• User interface for Windows 95/98/NT and some Windows CE machines

For more information, see their website at: http://www.iae.nl/users/aed/rdas/rdas.htm.