| |
|
 |
| GENERAL |
|
| wing
Span |
30
ft |
| Overall
length |
43
ft |
| Overall
Height |
19
ft |
| |
|
| POWER
PLANT |
|
| two
Rolls Royce/Pratt & Whitney |
|
| RTM
322 (coupled installation) |
|
| Max
Power: 5,600 ESHP |
|
| Best
Consumption |
0.41/lbs/hp/hr |
| |
|
| WEIGHTS
(approximate) |
|
| Takeoff
Weight |
18,000
lbs |
| Empty
Weight |
9,000
lbs |
| Useful
Load |
8,000
lbs |
| Max
Fuel (internal) |
2,200
lbs |
| Max
Fuel (external) |
3,800
lbs |
| bomb
bay tank |
3,000
lbs |
| |
|
| PERFORMANCE |
|
| Service
Ceiling |
20,000
ft |
| max
Speed |
420
kts |
| Normal
Cruise |
350
kts |
| Minimum
Speed |
10
kts |
| Rate
of Climb |
3,500
fpm |
| Max
"G" loading |
+8,
-4 |
| |
|
| FIELD
PERFORMANCE |
|
| Takeoff
over 50' obstacle |
under
100' |
| Landing
Roll |
under
100' |
| |
|
| RANGE |
|
| Operatonal
theater Range |
|
| 7,000
lbs Ordinance |
620
nm |
| Ferry
Range W/no payload |
|
| and
8,800 lbs fuel |
3,000
nm |
| |
|
| Update:
New NASA reasearch would appear to make the P-50 capable of VTOL,
and increase performance in all areas. |
|