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#11
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I know of no actual measurement of drag with the FES (i.e. with prop
folded) but there was some report of comparison flying in a comp with a similar glider of another make (Ventus?). Can’t recall the link now, but it would have been either in Lak’s website or Luka’s (the designer/ developer). For my money, any slight increase in drag is not only imperceptible to me, but is (a tiny) part of a price I am willing to pay for its advantages in my particular compromise – getting home without a retrieve crew if a cross country does not pan out, and getting away from virtually any launch if it is at all soarable, etc. Chris N. |
#12
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Hi Gang
I have had a DG800B and a Stemme S10VT for many years and currently have a Phoenix so I have some experience with self launchers. I almost purchased an Antares a couple of years ago but discovered a gotcha that for me was a show stopper. And that gotcha? Lithium batteries cannot exceed fairly modest temperatures before they have to be shutdown meaning if I left an Antares in the hot midday sun in Nevada for a couple of hours I might not even be able to reach 1,000 feet before the electric system would automatically shut down. This might be OK in cooler climates but not at Minden. The vibration problems of the DG require almost constant monitoring of the engine and its supports for wear and tear. The Wankel engine of the 26 is apparently much less prone to vibration problems. Anything using the Rotax engine is reliable. The Stemme had maintenance problems but the Rotax 914 engine was reliable. So if you want the highest performance single place self launcher I would recommend the Ventus or the 26. For a 2 place self launcher the Stemme is hard to beat with its much better ground handling compared to a 25 although the performance of the 25 is a little better. For a little old guy like me who has completed all the 6 hour XC flights he ever wants to do in the DG800B and the Stemme you might want to consider a touring motorgllider and there is one that clearly stands above the rest and that is the Phoenix. It is the first that allows the outer wing panels to be removed in less than a minute reducing the wing span from 15 meters to 11 meters thereby allowing the Phoenix to be parked in a regular hanger. In the short wing configuration it is a superb LSA power plane and in the long wing configuration it is a medium performance motorglider. It is registered as a LSA glider even though in the short wing configuration it is clearly a standard LSA power plane. The FAA had never considered this a possibility and a registered aircraft cannot have 2 certifications. That suits me. Dave |
#13
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At the lower cost end of the spectrum, I can say that the rotax
installation of the Apis is very well thought out and has performed for me over 4 seasons without fail for air restarts. It runs cool and usually requires less than a minute at idle before stowing. The engine is rev limited to about 6000 rpm and I don't always get that. It is relatively idiot proof, (witness I am still here writing). This particular installation is no longer available as AMS bit the dust. The glider is still being built by Pipistrelle with a different engine. The Apis is not a state of the art high aspect glider but capable of long cross country, have done 300k here in Oregon. The wing area is large, keeping the loading down, and while I get only 5-600 fpm at sea level, I still get a positive rate at 10k. Vibration is unpleasant, and I am constantly looking for the smoothest rpm range for the altitude, sometimes 100 rpm makes a huge difference. Nothing has shaken off the bird yet and I constantly tell myself, that it is at least as pleasant as flying around on tow. Not sure what Pipistrelle is asking but I got in for about 1/2 what a German machine would cost, including the trailer. Mark |
#14
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On Wednesday, January 11, 2012 1:24:33 PM UTC-5, kd6veb wrote:
... I almost purchased an Antares a couple of years ago but discovered a gotcha that for me was a show stopper. And that gotcha? Lithium batteries cannot exceed fairly modest temperatures before they have to be shutdown meaning if I left an Antares in the hot midday sun in Nevada for a couple of hours I might not even be able to reach 1,000 feet before the electric system would automatically shut down. This might be OK in cooler climates but not at Minden. Huh ? I regularly self-launch at Uvalde, Hobbs, etc. Not exactly locations I need the Sorel boots. Battery heating is the third power of current. Thus, reducing from max power shortly after take-off reduces heating enough that this has never been an issue for me in actual operation over many seasons (including multiple contests at Hobbs and Uvalde, launching on HOT days with full water ballast). Hope that's clear ! Best Regards, Dave "YO electric" |
#15
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On Jan 11, 12:19*pm, Dave Nadler wrote:
Battery heating is the third power of current. Really? Assuming no external heater is enabled isn't the power that heats the batteries the product of the internal resistance and the current and the current? ( I squared R, rather than I cubed R) Andy |
#16
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On Jan 10, 7:48*pm, key wrote:
I am curious what group members with experience with self-launchers regard as the best propulsion system (currently) in terms of in-flight restart reliability, maintenance, safety, and other operational factors (e.g., vibration). *Of course the electric Antares might win on all counts except for range, but it is out of my price league. thanks, Key NEW: Silent 2 ELECTRO FESL Front Electric Self Launch ease of operation and peace of mind greater reliability when compared with any internal combustion engine secure and instant start-up; the motor requires no warm-up prior to application of full power absence of vibration; the only moving parts are the propeller and the rotor maintenance is essentially unnecessary nose-mounted motor is on the fuselage center-line and thus has no forward pitching moment to create take-off difficulties as is typical of pylon mounted propellers no loss of motor power as a function of altitude; performance is unvaried with respect to atmospheric conditions motor use is extremely simple; no raising of a pylon, simply turn on the master and apply power absence of aerodynamic resistance (engine pylon, etc.) and consequently better flight performance simplicity and uncomplicated use of the entire system, when compared to solutions with a retractable no change to the aerodynamics when using the motor no change to the center of gravity when changing between powered and unpowered flight. prop located in front of the cockpit and safely visible to the pilot at all times availability of extra electric energy for even the most well-equipped instrument panel lowest price for a new glider can fly more then an hour level http://www.alisport.com/eu/eng/silent2electro.htm I WANT ONE!!!!! |
#17
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Seems like not much clearance between the prop and the runway. Probably
pretty expensive if you hit the runway with the prop. On 1/11/2012 12:16 PM, silentpilot wrote: On Jan 10, 7:48 pm, wrote: I am curious what group members with experience with self-launchers regard as the best propulsion system (currently) in terms of in-flight restart reliability, maintenance, safety, and other operational factors (e.g., vibration). Of course the electric Antares might win on all counts except for range, but it is out of my price league. thanks, Key NEW: Silent 2 ELECTRO FESL Front Electric Self Launch ease of operation and peace of mind greater reliability when compared with any internal combustion engine secure and instant start-up; the motor requires no warm-up prior to application of full power absence of vibration; the only moving parts are the propeller and the rotor maintenance is essentially unnecessary nose-mounted motor is on the fuselage center-line and thus has no forward pitching moment to create take-off difficulties as is typical of pylon mounted propellers no loss of motor power as a function of altitude; performance is unvaried with respect to atmospheric conditions motor use is extremely simple; no raising of a pylon, simply turn on the master and apply power absence of aerodynamic resistance (engine pylon, etc.) and consequently better flight performance simplicity and uncomplicated use of the entire system, when compared to solutions with a retractable no change to the aerodynamics when using the motor no change to the center of gravity when changing between powered and unpowered flight. prop located in front of the cockpit and safely visible to the pilot at all times availability of extra electric energy for even the most well-equipped instrument panel lowest price for a new glider can fly more then an hour level http://www.alisport.com/eu/eng/silent2electro.htm I WANT ONE!!!!! |
#18
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On 1/11/2012 1:33 PM, Greg Arnold wrote: (referring to the Alisport Silent 2
Electro) Seems like not much clearance between the prop and the runway. Probably pretty expensive if you hit the runway with the prop. Mercy!!! Pretty much true of all self-launching prop planes with which I'm familiar... YMMV, Bob W. |
#19
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That's what I would have guessed, but its
a bit more complicated than that... |
#20
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On Jan 11, 3:33*pm, Greg Arnold wrote:
Seems like not much clearance between the prop and the runway. *Probably pretty expensive if you hit the runway with the prop. new prop 2 grands???? not much clearance between the prop and the runway during the first 11 seconds, then the Silent is off the ground.......... I would hold the stick full back.. And never taxi. |
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