Scanlan SG-1A
# Scanlan SG-1A

The Scanlan SG-1A is an American, single seat, pod-and-boom, high-wing, strut-braced glider that was designed by Thomas W. Scanlan in 1970 and sold in the form of plans for amateur construction.

## Design and development

The SG-1 was conceived as a very simple and economical aircraft that could be built with modest construction skills and very little financial investment. The prototype was completed in 1970 for US$400 and subsequent aircraft were built for under US$1000.

The SG-1 is constructed with a welded steel fuselage and tail surfaces and covered with doped aircraft fabric. The wing is made from an aluminium structure, covered in aluminum sheet and features upper-surface spoilers and a modified Gö 549 airfoil. The landing gear is a monowheel with the forward fuselage protected by a skid. The airframe was static tested to 9g without failing.

With a very low stall speed of 32 mph (51 km/h), pilots who have flown the aircraft claim that the SG-1 can fly a thermal inside a Schweizer SGS 1-26.

## Operational history

In April 2011 there was one SG-1 and one SG-1A on the Federal Aviation Administration registry.

## Variants

### SG-1

    Prototype design, with V-struts and a constant-chord wing. One built.

### SG-1A

    Improved model, with double-tapered wings and single wing struts. About four built.

## Aircraft on display

* US Southwest Soaring Museum

## Specifications (SG-1A)

Data from Sailplane Directory and Soaring

General characteristics

* Crew: one
* Wingspan: 40 ft 0 in (12.19 m)
* Wing area: 125 sq ft (11.6 $m^2)$
* Aspect ratio: 15.4:1
* Airfoil: modified Gö 549
* Empty weight: 300 lb (136 kg)
* Gross weight: 550 lb (249 kg)

Performance

* Stall speed: 32 mph (51 km/h, 28 kn)
* Never exceed speed: 100 mph (160 km/h, 87 kn)
* Maximum glide ratio: 20:1 at 55 mph (89 km/h)
* Rate of sink: 180 ft/min (0.91 m/s) at 47 mph (76 km/h)
* Wing loading: 4.4 lb/sq ft (21 $kg/m^2)$
