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#1
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mr1956 wrote in
: .... I have been reading the ARRL antenna book and while there is much information, a lot of it is over my head. But one point I think a chapter makes is that a 1/4 wave monopole will work better than a 1/2 wave using an artificial ground plane because of the way the voltage peaks at the end of the antenna; or that is how it seems. Your transmitter is designed for a particular load impedance, almost certainly 50 ohms... check the specs. The load presented to the transmitter terminals depends on the feed point impedance of the antenna, and impedance transformation that may occur on the coaxial feedline. In the case you describe, the *antenna system* design was most unsuited to a 50 ohm transmitter, hence the considerable loss predicted. Your newer proposal for a quarter wave wire perpedicular to the rocket body with the coax shield connected to the metallic rocket body is not exactly 50 ohms, but probably close enough that antenna system efficiency will be fairly good and the transmitter should deliver most of its rated power. Owen |
#2
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On May 24, 5:49*pm, Owen Duffy wrote:
mr1956 wrote : ... I have been reading the ARRL antenna book and while there is much information, a lot of it is over my head. *But one point I think a chapter makes is that a 1/4 wave monopole will work better than a 1/2 wave using an artificial ground plane because of the way the voltage peaks at the end of the antenna; or that is how it seems. Your transmitter is designed for a particular load impedance, almost certainly 50 ohms... check the specs. The load presented to the transmitter terminals depends on the feed point impedance of the antenna, and impedance transformation that may occur on the coaxial feedline. In the case you describe, the *antenna system* design was most unsuited to a 50 ohm transmitter, hence the considerable loss predicted. Your newer proposal for a quarter wave wire perpedicular to the rocket body with the coax shield connected to the metallic rocket body is not exactly 50 ohms, but probably close enough that antenna system efficiency will be fairly good and the transmitter should deliver most of its rated power. Owen What I have been finding out is developing a matching circuit for the output of the transmitter is not easy, at least for me and at that frequency. It could be done if I was a cell phone manufacturer. I think much will be gained by using the 1/4 wave as opposed to the 1/2 wave on the airframe and a yagi or helix antenna on the ground station. I will post a link to some images of the project when I have time. Information on the flight can be found at www.lokiresearch.com and look for information about the Proteus 6 flight at the Balls 17 event, Black Rock, NV September 2008. I'll also add some thoughts about how I intend to proceed based on everyone's great input from this forum. One quick question: Am I correct in assuming that the ground lead of the rocket mounted antenna should be as short as possible? i.e., the connection between the shield of the RG-178 and the metal airframe. Thanks, Curt |
#3
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On Mon, 25 May 2009 09:48:23 -0700 (PDT), mr1956
wrote: One quick question: Am I correct in assuming that the ground lead of the rocket mounted antenna should be as short as possible? i.e., the connection between the shield of the RG-178 and the metal airframe. Very much so - mm instead of inches. 73's Richard Clark, KB7QHC |
#4
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mr1956 wrote in
: .... What I have been finding out is developing a matching circuit for the output of the transmitter is not easy, at least for me and at that frequency. It could be done if I was a cell phone manufacturer. I think much will be gained by using the 1/4 wave as opposed to the 1/2 wave on the airframe and a yagi or helix antenna on the ground station. The easy solution is the one I suggested. I will post a link to some images of the project when I have time. Information on the flight can be found at www.lokiresearch.com and look for information about the Proteus 6 flight at the Balls 17 event, Black Rock, NV September 2008. I'll also add some thoughts about how I intend to proceed based on everyone's great input from this forum. One quick question: Am I correct in assuming that the ground lead of the rocket mounted antenna should be as short as possible? i.e., the connection between the shield of the RG-178 and the metal airframe. Loss on the coax can be much worse when it is mismatched. I gave you figures for a 2000 ohm load (representing your end fed half wave antenna). The loss for 0.3m with a 30 ohm load is 0.5dB, it is 90% efficient. If you shorten it, you will reduce the loss, but I wouldn't obsess over it. The problem you have right now is due principally to high standing waves on the line and unsuitable transmitter load, and you solve much of that using a quarter wave antenna. Without a diagram, we are at great risk of misunderstanding. If you cannot affort the time to invest in making a drawing, you take the risk of misinterpretation of your words. The connection from the shield to the metal air frame and presumably metal skin should be short. Regard that the effective length of the antenna in that case is the distance from the shield to the tip of the whip. Owen |
#5
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On May 25, 5:26*pm, Owen Duffy wrote:
mr1956 wrote : ... What I have been finding out is developing a matching circuit for the output of the transmitter is not easy, at least for me and at that frequency. It could be done if I was a cell phone manufacturer. *I think much will be gained by using the 1/4 wave as opposed to the 1/2 wave on the airframe and a yagi or helix antenna on the ground station. The easy solution is the one I suggested. I will post a link to some images of the project when I have time. Information on the flight can be found atwww.lokiresearch.comand look for information about the Proteus 6 flight at the Balls 17 event, Black Rock, NV September 2008. I'll also add some thoughts about how I intend to proceed based on everyone's great input from this forum. *One quick question: Am I correct in assuming that the ground lead of the rocket mounted antenna should be as short as possible? i.e., the connection between the shield of the RG-178 and the metal airframe. Loss on the coax can be much worse when it is mismatched. I gave you figures for a 2000 ohm load (representing your end fed half wave antenna).. The loss for 0.3m with a 30 ohm load is 0.5dB, it is 90% efficient. If you shorten it, you will reduce the loss, but I wouldn't obsess over it. The problem you have right now is due principally to high standing waves on the line and unsuitable transmitter load, and you solve much of that using a quarter wave antenna. Without a diagram, we are at great risk of misunderstanding. If you cannot affort the time to invest in making a drawing, you take the risk of misinterpretation of your words. The connection from the shield to the metal air frame and presumably metal skin should be short. Regard that the effective length of the antenna in that case is the distance from the shield to the tip of the whip. Owen OK, I think I know generally how to proceed from here. FYI, some images of the previous design can be found at the following URLs: http://i647.photobucket.com/albums/u...9/Curtjeff.jpg http://i647.photobucket.com/albums/u...09/liftoff.jpg http://i647.photobucket.com/albums/u.../Coupler02.jpg http://i647.photobucket.com/albums/u...009/Elec05.jpg http://i647.photobucket.com/albums/u...ery04small.jpg This one is an image of the type of gear I normally work with: http://i647.photobucket.com/albums/u.../Guam02004.jpg So the key points are as follows: 1. Fabricate a 1/4 wave antenna and mount that is totally exterior to the metal airfame and terminate the coax as close as possible to the antenna. 2. I imagine that I could start off with a longer than needed whip antenna, then trim it back while taking measurements with the RF millivolt meter until it looks like I've gotten maximum signal strength. 3. Use either a helix or yagi receiving antenna on the ground station to boost the signal strength on the receiving end. I accept that words alone are not always sufficient to describe such things but I think the important issues have been well described by everyone here. I can only make the RG-178 whip connecting the transmitter to the antenna so short, as I need sufficient length to remove the electronics from inside of the avionics compartment to change batteries,etc. But I think the critical issues are having a direct and solid electrical connection between the antenna and coax and using a higher db antenna on the receiving end; the ground based antenna may make the most difference in the end. I'll have to go back and look at the posts to make sure I've gotten all of the information right and if anyone has any more questions after reviewing the images please let me know and I will respond as needed. Also, there should be an article coming out in Smithsonian Air & Space magazine in the "Above and Beyond" section sometime in the future describing this particular flight and more information is online at www.lokiresearch.com (the Proteus 6 flight). Curt |
#6
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![]() "mr1956" wrote ... On May 25, 5:26 pm, Owen Duffy wrote: mr1956 wrote : What I have been finding out is developing a matching circuit for the output of the transmitter is not easy, at least for me and at that frequency. It could be done if I was a cell phone manufacturer. I think much will be gained by using the 1/4 wave as opposed to the 1/2 wave on the airframe and a yagi or helix antenna on the ground station. The easy solution is the one I suggested. I will post a link to some images of the project when I have time. Information on the flight can be found atwww.lokiresearch.comand look for information about the Proteus 6 flight at the Balls 17 event, Black Rock, NV September 2008. I'll also add some thoughts about how I intend to proceed based on everyone's great input from this forum. One quick question: Am I correct in assuming that the ground lead of the rocket mounted antenna should be as short as possible? i.e., the connection between the shield of the RG-178 and the metal airframe. Loss on the coax can be much worse when it is mismatched. I gave you figures for a 2000 ohm load (representing your end fed half wave antenna). The loss for 0.3m with a 30 ohm load is 0.5dB, it is 90% efficient. If you shorten it, you will reduce the loss, but I wouldn't obsess over it. The problem you have right now is due principally to high standing waves on the line and unsuitable transmitter load, and you solve much of that using a quarter wave antenna. Without a diagram, we are at great risk of misunderstanding. If you cannot affort the time to invest in making a drawing, you take the risk of misinterpretation of your words. The connection from the shield to the metal air frame and presumably metal skin should be short. Regard that the effective length of the antenna in that case is the distance from the shield to the tip of the whip. Owen OK, I think I know generally how to proceed from here. FYI, some images of the previous design can be found at the following URLs: http://i647.photobucket.com/albums/u...9/Curtjeff.jpg http://i647.photobucket.com/albums/u...09/liftoff.jpg http://i647.photobucket.com/albums/u.../Coupler02.jpg http://i647.photobucket.com/albums/u...009/Elec05.jpg http://i647.photobucket.com/albums/u...ery04small.jpg This one is an image of the type of gear I normally work with: http://i647.photobucket.com/albums/u.../Guam02004.jpg So the key points are as follows: 1. Fabricate a 1/4 wave antenna and mount that is totally exterior to the metal airfame and terminate the coax as close as possible to the antenna. 2. I imagine that I could start off with a longer than needed whip antenna, then trim it back while taking measurements with the RF millivolt meter until it looks like I've gotten maximum signal strength. 3. Use either a helix or yagi receiving antenna on the ground station to boost the signal strength on the receiving end. I accept that words alone are not always sufficient to describe such things but I think the important issues have been well described by everyone here. I can only make the RG-178 whip connecting the transmitter to the antenna so short, as I need sufficient length to remove the electronics from inside of the avionics compartment to change batteries,etc. But I think the critical issues are having a direct and solid electrical connection between the antenna and coax and using a higher db antenna on the receiving end; the ground based antenna may make the most difference in the end. I'll have to go back and look at the posts to make sure I've gotten all of the information right You miss the most important. Helmut wrote "Do not use too thin wires, the thicker the better." and if anyone has any more questions after reviewing the images please let me know and I will respond as needed. Also, there should be an article coming out in Smithsonian Air & Space magazine in the "Above and Beyond" section sometime in the future describing this particular flight and more information is online at www.lokiresearch.com (the Proteus 6 flight). S* |
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