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SGM 2-37

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Listing Description

The SGM 2-37 self-launching motorglider, which
first flew in 1982, has the capacity to operate
as a towplane for other gliders. 9 (known as the
TG-7A) are operated as trainers at the U.S. Air
Force Academy. The aircraft is without flaps but
has balanced upper/lower surface dive brakes. ATC

Performance

L/DMax 28 MinSink 0.96 m/s / 3.16 fps / 1.87 kt

Specifications

Aspect ratio

17.9

Span

18.14 m 59.5 ft

Area

18.18 sq.m 195.7 sq.ft

Empty Weight

544 kg 1200 lb.

Payload

213 kg 470 lb.

Gross Weight

757 kg 1670 lb.

Wing Load

41.64 kg/sq.m 8.99 lb./sq.ft

Water Ballast

0 kg 0 lb.

General Details

Manufacturer Schweizer Plane Name SGM 2-37 Classification Unclassified Country Of Origin U S A Designer Leslie Schweizer No. of Seats 2 No. Built 12 Airfoil Wortmann Fx 61-163 Structure all metal Engine 83 kW/ 112 bhp Lycoming 0-235-L2C

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SGM 2-37

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