On Wednesday, March 17, 2021 at 9:00:04 AM UTC-4, Eric Greenwell wrote:
2G wrote on 3/16/2021 10:17 PM:
On Tuesday, March 16, 2021 at 3:48:54 PM UTC-7, Eric Greenwell wrote:
2G wrote on 3/16/2021 12:46 PM:
Landing out in eastern Nevada is serious business; some may chose to fly non-motorized gliders there (which, in my mind, the GP15 is) and get away with it.
I forgot to respond to the "non-motorized" portion of your remarks. Perhaps you will be
surprised (or at least interested) to learn the GP15 climb rate from the runway on a typical
flying day at Ely will be nearly double the climb rate of my ASH26E. A major reason is the
electric motor still has the same power at 9000' DA, while the carbureted Wankel has lost about
18%. The better climb on takeoff in high density altitudes was an important factor in my
choice. It's not important at Ely, but it is at Parowan, and a few other places I've flown (or
wanted to fly but decided it was marginal).

Now, I realize you think 90 miles of self-retrieve is the same as zero miles, but that view is
not shared by every "pure" glider pilot out there!
--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me)
- "A Guide to Self-Launching Sailplane Operation"
https://sites.google.com/site/motorg...ad-the-guide-1

Where do you get 90 miles? GP's website doesn't list it. Their numbers are dry - if you can trust them (nobody's verified them and they may be estimated for all you know). The self-retrieve distance they list for the B battery is 100km (63 miles) with a 800m launch with no ballast. Now add ballast, add an 3,000 ft obstacle and a 20kt headwind (all realistic conditions at Ely) and refigure what the hypothetical retrieve distance is, if any.

Take a look at this page: https://www.gpgliders.com/offer/gp-15-e-se-jeta Here's the pertinent
portion:

Usable battery capacity: 9,23 kWh
Operational battery capacity: 8,36 kWh (10% buffer to preserve battery life)
Weight: 52 kg (115 lb)

Motor glider’s self-launch and climb performance on a single charge, equipped with “B” battery
pack (TOW: 320 kg [705 lb]):

5 x take-off and climb to 800 m (2 625 ft) altitude
or 1 x take-off and climb to 800 m (2 625 ft) altitude + 150 km (93 mi) range
or 1 x take-off and total climb to 4 000 m (13 120 ft)
Max. climb rate: 4,4 m/s (8,55 kts)
Ground-roll take-off distance: 180 m (197 yards)

Because the wing area is 84 ft2, the 705lb TOW = 8.4 lb/ft2, about the same wing loading I have
in the ASH26E, unballasted.
--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me)
- "A Guide to Self-Launching Sailplane Operation"
https://sites.google.com/site/motorg...ad-the-guide-1

Eric, I'm curious about the wing loadings quoted for the Jeta from 7,58-13,72 lb/ft^2. For the conditions I fly in Ontario where thermals average 2 to 4 kts, I see these heavy wing loadings as a disadvantage even in a flapped ship. I fly my D2 mostly dry at less than 6 lb/ft^2. What am I missing?
Ian IN