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In parallel with the specification to which the La-168
was to be developed, a requirement was formulated for
a lighter "frontal fighter" powered by the Rolls-Royce
Derwent turbojet. To meet the latter demand, the
Lavochkin bureau evolved two designs, the La-172 and
the La-174TK. The former was effectively a scaleddown
version of the La-168 tailored for the lower-powered,
smaller engine and the latter featured exceptionally
thin, unswept wings and a configuration
generally similar to that of the earlier La-152 series of
fighters. The La-172 was powered by an NII-1 turbojet
(as the pre-series Soviet version of the Derwent was designated)
rated at 1600kg, and entered
flight test early in 1948, with armament comprising
three 23-mm NS-23 cannon. Early in the test programme,
while being flown by I Ye Fedorov, the La-172
suffered uncontrollable flutter at 8000m and
entered a flat spin. Recovery was effected at 3000m, but the prototype was heavily damaged in a
subsequent crash landing. Nevertheless, development
was continued via the La-174D to result in the La-15.
| WEIGHTS |
| Take-off weight | 3708 kg | 8175 lb |
| Empty weight | 2433 kg | 5364 lb |
| DIMENSIONS |
| Wingspan | 8.83 m | 28 ft 12 in |
| Length | 9.56 m | 31 ft 4 in |
| Wing area | 16.16 m2 | 173.94 sq ft |
| PERFORMANCE |
| Max. speed | 1040 km/h | 646 mph |
| Range | 1300 km | 808 miles |
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