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- From: billn@hpcvaac.cv.hp.com (bill nelson)
- Subject: Re: Tracking
- Message-ID: <1993Jan27.002254.21349@hpcvaac.cv.hp.com>
- Organization: Hewlett-Packard Company, Corvallis, Oregon USA
- References: <JASON.93Jan26152521@ab20.larc.nasa.gov>
- Date: Wed, 27 Jan 1993 00:22:54 GMT
- Lines: 36
-
- jason@ab20.larc.nasa.gov (Jason Austin) writes:
-
- : I once saw a device at a hobby shop to help with this problem.
- : You put a small transmitter in the rocket and keep a gun shaped
- : detector on the ground. The gun beeps louder depending on how how
- : directly you're pointing it at the transmitter. I think that set was
- : around $30. I don't remember what kind of range they claimed.
-
- That is an audio tracker - it is only good for a few hundred feet. I seem
- to recall that Estes says 100 feet, but am not sure. It is overpriced.
- You can buy a buzzer and battery for a few dollars for the "transmitter".
- You can use a plastic funnel, costing another couple of dollars, for the
- "receiver". Not elegant, but just as good. It is useless for "out of sight"
- rockets.
-
- : -> BTW, does anyone know the decent rate of a 1lb rocket with an 18" chute? I
- : -> guessed that it took about 90 seconds for the rocket to land with the chute.
- : -> With about a 25 mph wind that puts the rocket at (25mph * (90s/(3600 sec/hr)))
- : -> .625 mi from where I launched it. So that was where I concentrated the search.
- : ->
- : -> Thanks in advance for any help :)
- :
- : I believe this will vary greatly depending on the shape of the
- : rocket and the parachute.
-
- It would depend most on the drag coefficient of the chute. There are
- equations for calculating the rate. I think there was an article in
- the Tripolitan (High Power Rocketry Magazine). There is also a book
- that was written by a rocketeer covering the subject. I do not recall
- the title or who has it for sale. Maybe someone else will remember.
-
- The shape of the rocket has nothing to do with the descent rate. It
- has negligible lift at descent rates.
-
- Bill
-
-