IS-28 Description
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The IS-28 design team leader was Iosef Silimon. The IS-28B2 first flew in Romania in 1973. The IS-28B2 is an all-metal sailplane with a wing span of 17m. The wing profile has Wortmann low drag aerofoils, and the wing is fitted with flaps and air brakes. The low drag fuselage has a semi-retractible mainwheel.

Technical Data
| Item |
Value |
| Span |
17 m. |
| Wing Area |
18.24 sq. m. |
| Aspect Ratio |
15.8 |
| Length |
8.17 m. |
| Aerofoil |
Wortmann FX61-163, FX60-126 |
| Empty Mass |
330 kg. |
| Max Mass |
590 kg. |
| Wing Loading |
32.34 kg/m2 |
| Maximum speed (Vne) |
266 km/hr |
| Best glide ratio |
34:1 |
| Minimum sink |
0.69 m/sec |