|
|
In May 1944, Curtiss indicated to the AAF that it
wished to abandon further work on the P-60 series
fighters because of the disappointing results achieved
with the XP-60C and XP-60E. Earlier, the P-60 had been
eliminated from the production schedules, the number
of aircraft on contract having been reduced to two.
However, the AAF insisted on completion of one of the
two aircraft still on order. These, originally ordered as
YP-60As, had been redesignated as YP-60Es because
the design modifications incorporated were most
directly descended from the XP-60E. The YP-60E differed
principally in having a 2,100hp R-2800-18 engine,
a deeper cowling incorporating the ventral cooler intake,
a cut-down rear fuselage and a bubble-type cockpit
canopy. The sole YP-60E completed was flown on 13
July 1944, but only one further flight was made before
the aircraft was transferred to Wright Field where it
was eventually disposed of without further testing.
Armament comprised six wing-mounted 12.7mm machine guns.
 | A three-view drawing (1278 x 966) |
| WEIGHTS |
| Take-off weight | 4 658 kg | 9 lb |
| Empty weight | 3 758 kg | 7 lb |
| DIMENSIONS |
| Wingspan | 12.60 m | 41 ft 4 in |
| Length | 10.34 m | 33 ft 11 in |
| Height | 3.81 m | 12 ft 6 in |
| Wing area | 22.55 m2 | 242.73 sq ft |
| PERFORMANCE |
| Max. speed | 652 km/h | 405 mph |
|
Do you have any comments about this aircraft ?
|
| |