cjl
22-July-2007, 06:37 AM
Well, as many of you know (and I'm sure many others guessed based on my avatar), I am fairly heavily into high power rocketry, and have been flying rather large rockets for some time.
However, until today, they have all been subsonic. Today, I finally got a rocket supersonic without breaking or losing it :D
The rocket was a 1.6 inch diameter, 44 inch long rocket that weighed 479 grams. The motor was an Aerotech I600R, which is also 1.6 inches in diameter, is 13 inches long, and weighs 617 grams loaded (323.7g of propellant). It has a total impulse of around 640 Ns. Here are a few graphs taken from the altimeter that was onboard to record the flight (they're large images, but small files - only about 40kb each):
First, the acceleration graph
The sudden drop in deceleration around 3.6 seconds is because it is dropping subsonic, creating a dramatic reduction in drag. Also, the huge spike at about 22 seconds is the shock of the deployment of the parachute:
http://i27.photobucket.com/albums/c183/chris_lapanse/Accelerationgraph.png
Next, a graph of velocity:
http://i27.photobucket.com/albums/c183/chris_lapanse/Velocitygraph.png
The next two are both altitude graphs, but were obtained slightly differently. The first is an integrated altitude graph, which was obtained by taking the second integral of the measured acceleration values - it is more accurate throughout the mach region, but may be slightly less accurate for peak altitude, as it cannot account for a slightly nonvertical flight:
http://i27.photobucket.com/albums/c183/chris_lapanse/Integratedaltgraph.png
Finally, the barometric altitude graph. This one isn't perfectly calibrated yet (the altimeter is an experimental one), but should be fairly close. In addition, I think it's pretty neat to see the effects that the mach transitions had on the reading - look at the inconsistencies around 0.4 seconds (when it first entered mach) and then later at about 3.6 seconds, when it was slowing from supersonic to subsonic again. Kind of neat to see:
http://i27.photobucket.com/albums/c183/chris_lapanse/Baroaltgraph.png
Now, if anyone is still reading, the pretty pictures (these ones are clickable thumbnails because the filesize is MUCH larger):
Here is the rocket right at ignition:
http://s27.photobucket.com/albums/c183/chris_lapanse/th_RG1S3362crop.jpg (http://i27.photobucket.com/albums/c183/chris_lapanse/RG1S3362crop.jpg)
And here it is screaming off on its way to mach 1.6 and over 3000 meters:
(it's already doing about 60m/s in this picture)
http://s27.photobucket.com/albums/c183/chris_lapanse/th_RG1S3363crop.jpg (http://i27.photobucket.com/albums/c183/chris_lapanse/RG1S3363crop.jpg)
If and when I get better calibration data for the barometric sensor, I'll post the updated numbers, and I also have a picture of me with the rocket somewhere around here. I'll get those up sometime tomorrow. I'm absolutely thrilled though - I've been wanting to do this for several years now, and have destroyed a couple rockets and lost a couple more trying to achieve it :)
However, until today, they have all been subsonic. Today, I finally got a rocket supersonic without breaking or losing it :D
The rocket was a 1.6 inch diameter, 44 inch long rocket that weighed 479 grams. The motor was an Aerotech I600R, which is also 1.6 inches in diameter, is 13 inches long, and weighs 617 grams loaded (323.7g of propellant). It has a total impulse of around 640 Ns. Here are a few graphs taken from the altimeter that was onboard to record the flight (they're large images, but small files - only about 40kb each):
First, the acceleration graph
The sudden drop in deceleration around 3.6 seconds is because it is dropping subsonic, creating a dramatic reduction in drag. Also, the huge spike at about 22 seconds is the shock of the deployment of the parachute:
http://i27.photobucket.com/albums/c183/chris_lapanse/Accelerationgraph.png
Next, a graph of velocity:
http://i27.photobucket.com/albums/c183/chris_lapanse/Velocitygraph.png
The next two are both altitude graphs, but were obtained slightly differently. The first is an integrated altitude graph, which was obtained by taking the second integral of the measured acceleration values - it is more accurate throughout the mach region, but may be slightly less accurate for peak altitude, as it cannot account for a slightly nonvertical flight:
http://i27.photobucket.com/albums/c183/chris_lapanse/Integratedaltgraph.png
Finally, the barometric altitude graph. This one isn't perfectly calibrated yet (the altimeter is an experimental one), but should be fairly close. In addition, I think it's pretty neat to see the effects that the mach transitions had on the reading - look at the inconsistencies around 0.4 seconds (when it first entered mach) and then later at about 3.6 seconds, when it was slowing from supersonic to subsonic again. Kind of neat to see:
http://i27.photobucket.com/albums/c183/chris_lapanse/Baroaltgraph.png
Now, if anyone is still reading, the pretty pictures (these ones are clickable thumbnails because the filesize is MUCH larger):
Here is the rocket right at ignition:
http://s27.photobucket.com/albums/c183/chris_lapanse/th_RG1S3362crop.jpg (http://i27.photobucket.com/albums/c183/chris_lapanse/RG1S3362crop.jpg)
And here it is screaming off on its way to mach 1.6 and over 3000 meters:
(it's already doing about 60m/s in this picture)
http://s27.photobucket.com/albums/c183/chris_lapanse/th_RG1S3363crop.jpg (http://i27.photobucket.com/albums/c183/chris_lapanse/RG1S3363crop.jpg)
If and when I get better calibration data for the barometric sensor, I'll post the updated numbers, and I also have a picture of me with the rocket somewhere around here. I'll get those up sometime tomorrow. I'm absolutely thrilled though - I've been wanting to do this for several years now, and have destroyed a couple rockets and lost a couple more trying to achieve it :)