|
|
Destined to be the last aircraft produced by the Lavochkin
design bureau, the La-250, known unofficially as
the Anaconda, was designed to meet a very demanding
1954 requirement for an ultra long-range, high-altitude
single-seat super interceptor armed exclusively with
missiles. Featuring a 57° delta wing and an enormous
fuselage of near-constant cross section, the
La-250 was powered by two Lyulka AL-7F turbojets
each rated at 6500kg which were later
to be fitted with afterburners boosting thrust to
9000kg. All control surfaces were fully
powered with duplex systems and without manual reversion.
Intended to carry the 30km acquisition-
range Uragan (Hurricane) radar, the La-250 had a
planned armament of two large K-15 beam-riding missiles.
Although the La-250 was intended as a single-seater
in operational form, prototypes were completed as two-seaters to provide accommodation for a test observer, and the first of three flying examples was
completed in July 1956. The first flight was attempted
on 16 July, but the test pilot, A G Kochetkov, encountered
an unexpectedly rapid roll moment and lost control.
Extensive testing of a systems rig followed before
acceptable characteristics were attained and flight
testing could be resumed. The second aircraft was lost
in a landing accident on 28 November 1957, and the
third aircraft also suffered a landing accident on 8 September
1958. The flight test programme suffered continual
delays as a result of poor engine reliability and
the full testing had not been completed when the programme
was cancelled.
| WEIGHTS |
| Take-off weight | 30000 kg | 66139 lb |
| Empty weight | 15000 kg | 33070 lb |
| DIMENSIONS |
| Wingspan | 13.90 m | 45 ft 7 in |
| Length | 25.60 m | 83 ft 12 in |
| Wing area | 80.0 m2 | 861.11 sq ft |
| PERFORMANCE |
| Max. speed | 2000 km/h | 1243 mph |
| Ceiling | 18000 m | 59050 ft |
| Range | 2000 km | 1243 miles |
 | A three-view drawing (1648 x 1073) |
Sg.KAR98, 08.03.2008 If Soviet Union had a different mind from capitalism,why only Sukhoi and Mikoyan Gurevich produced fighters in that time?
|
|
Do you have any comments concerning this aircraft ?
|
|  COMPANY PROFILE
FACTS AND FIGURES© The third La-250 had its nose
lowered by six degrees to give
better visibility on landing,
the poor view forward having
been determined as a factor in
the second crash. © Intended as a single-seater,
the prototypes had a second
seat for a flight test engineer. © Intended armament was a pair of
K-15 missiles that rode the beam
of the Uragan radar, which had a
range of 30km. © The missiles were cancelled
and the radar never made it
into an aircraft before the
development was cut short.
| |
|
|