SCHWEIZER SGS 2-32 Civil Aircraft Model Details

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General Information of SCHWEIZER SGS 2-32

Designer : Ernest Schweizer[1]

First Flight : 3 July 1962[2]

Manufacturer : Schweizer Aircraft Corporation

National Origin : United States

Number Built : 87

Role : Open-class sailplane

General characteristics of SCHWEIZER SGS 2-32

Aspect Ratio : 18.05

Airfoil : Root – NACA 633618, Mid – NACA 633618, Tip NACA 43 012A

Capacity : two passengers

Crew : one

Empty Weight : 831 lb (377 kg) equipped

Gross Weight : 1,430 lb (649 kg) Above 608 kg (1340 lb) only utility class

Height : 4 ft 0 in (1.22 m) at cockpit

Length : 26 ft 9 in (8.15 m)

Wing Area : 180 sq ft (16.7 m2)

Wingspan : 57 ft 0 in (17.37 m)

Performance of SCHWEIZER SGS 2-32

G Limits : +5.8 -3.8 at 164.0mph; 142.5kn (264km/h)

Maximum Glide Ratio : 35 at 55.9mph; 48.6kn (90km/h)

Never Exceed Speed : 157mph; 136kn (252km/h)

Rate Of Sink : 124ft/min (0.63m/s) at 46.0mph; 40.0kn (74km/h)

Stall Speed : 46mph (40kn; 74km/h)

Wing Loading : 6.0lb/sqft (29.3kg/m2)

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