Now many of you know I am part of this group involved with the Titanium Autogyro. However I fly and evaluate many machines of all kinds. This list below gives my findings as a test pilot.
Titanium autogyro test data:
Model: Titanium Explorer
Motor: Rotax 914
Prop: Bolly
Rotor: impregnated carbon fiber 9 inch cord x 28 feet
Conditions:
Temp 88 F
Field elevation 800 ft MSL
Density altitude 2000 ft
Wind 10 KTS
Total fuel 10 gal
Total pilot & passenger weight 485
Testing Pilot: CFI Desmon Butts
Rate of climb 500 ft per min.
VX: 55 KTS
Best glide : 55KTS
Cruise:70 KTS 5000 RPM fully loaded.
VNE 100 knots
More Data will be shown as testing continues.
This gyro is a joy to fly. The carbon blades have a smooth feel and a little more float but still have a sporty attitude.
I find the response with two people to be exceptional. Climb out with full load seemed to be almost effortless. Slight pressure to the left was compensated by a yolk trim system that is included. Landing is smooth with a special shock absorbing front geer. The front wheel design has slight semi castering qualities incase of side loading. However it is not prone to wheel shimmy. The rear spar also includes a small nylon tail wheel to prevent nose high flair tail damage.
The base empty weight is less then other models of similar make. This gives the Titanium Autogyro a higher useful load. This can be of course used for cargo or make it one of the few machines to carry larger passengers. The extras and attention to detail put it in a class of its own. Several features include: Duel prerotaor systems, adjustable peddles, rear glove box, cargo pods, prop rock guard, and many other finishing touches. All of these including the full gyro cover are standard equipment.
Wed Jun 03, 2015 8:52 pm
Gabor
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Outstanding! Thank you for the report. Waiting for more to come.
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Wed Jun 03, 2015 9:02 pm
Always Gone
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I spent a wonderful day flying in Newton Kansas. We flew the 914 turbo Titanium Explorer with an elevation of 1500. Density altitude 3400. Temp about 87 f. Full load and had a 13 kt headwind. Rate of climb 450ft per min.
Next week at 4500 ft we will use another entry.
I want a very clear performance picture of this aircraft in full load configuration.
Sat Jun 06, 2015 10:36 pm
MadMuz
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It would be useful to know pilot/passenger weights and fuel load when expressing rate of climb numbers. A nice density altitude number would also be helpful.
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_________________ Jon Carleton Private ASEL Instrument Sport Pilot Gyroplane
Sun Jun 07, 2015 7:54 pm
Arnie M.
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It would be useful to know pilot/passenger weights and fuel load when expressing rate of climb numbers. A nice density altitude number would also be helpful.
As Gabriel Iglesias would say on his fatness scale of 1 to 6 this one is #6 "Oh hell no!"
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Sun Jun 07, 2015 9:04 pm
Always Gone
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Actually Joe I thought I did list density altitude. As for the weight it was the same as the original post at the top. In the morning I will be getting the numbers for the high altitude stuff. I got to Brigham City today. I am trying to key all things the same where possible except of course field location. Any conditions, altitude , wind and density altitude will be noted.
Tue Jun 09, 2015 12:43 am
JonCarleton
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You likely did list density altitude or the components to make the calculation. I should go back and re-read. My comment was based on a line I read that extolled the two-place performance without passenger specifications.
I admit, being large-frame, to being sensitive to climb performance numbers. I have not been 170 pounds since 7th grade and when last I was at 2% body fat, I still weighed 225.
_________________ Jon Carleton Private ASEL Instrument Sport Pilot Gyroplane
Tue Jun 09, 2015 9:27 am
MadMuz
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You likely did list density altitude or the components to make the calculation. I should go back and re-read. My comment was based on a line I read that extolled the two-place performance without passenger specifications.
I admit, being large-frame, to being sensitive to climb performance numbers. I have not been 170 pounds since 7th grade and when last I was at 2% body fat, I still weighed 225.
Maybe you were actually 195# and the other 30# was your wallet
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Tue Jun 09, 2015 10:29 am
Arnie M.
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You likely did list density altitude or the components to make the calculation. I should go back and re-read. My comment was based on a line I read that extolled the two-place performance without passenger specifications.
I admit, being large-frame, to being sensitive to climb performance numbers. I have not been 170 pounds since 7th grade and when last I was at 2% body fat, I still weighed 225.
Your Long Horn would also reduce the rate of climb
Haaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaa
Tue Jun 09, 2015 12:35 pm
farmer jim
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You likely did list density altitude or the components to make the calculation. I should go back and re-read. My comment was based on a line I read that extolled the two-place performance without passenger specifications.
I admit, being large-frame, to being sensitive to climb performance numbers. I have not been 170 pounds since 7th grade and when last I was at 2% body fat, I still weighed 225.
Your Long Horn would also reduce the rate of climb
Haaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaa
NO PICTURES !!!!
fj
Sat Jun 13, 2015 8:28 am
MadMuz
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