| P-51
Specifications |
| |
|
|
Airframe Dimensions |
|
| |
|
| Wingspan |
:
25' 4.750" |
| Tailspan
|
:
106 " |
| Length
|
:
22' 6.000" |
| Height
at spinner |
:
72" |
| Shoulder
width front seat |
:
20" at shoulder / 24.5" at elbow |
| Shoulder
width rear seat |
:
19.5" at shoulder / 22.5" at elbow |
| Vertical
distance seat pan to inside of canopy in front seat |
:
41" |
| Vertical
distance seat pan to inside of canopy in rear seat / TF canopy
|
:
39" |
| Vertical
distance seat pan to inside of canopy in rear seat / D canopy
|
:
35" |
| Empty
weight (dependent upon option selection) |
:
1800 lbs |
| Gross
weight |
:
2500 lbs |
| Airfoil
design |
:
Roncz Special |
| Wing
area |
:
111 sq ft |
|
Wing loading |
:
22.5 lbs / sq ft |
| G
limits at gross weight |
:
6 positive / 4 negative |
| |
|
| Capacities
|
|
| |
|
| Fuel
capacity, wing tanks (30 gallons per side) |
:
60 gallons |
| Fuel
capacity, drop tanks (12 gallons per side) |
:
24 gallons |
| Engine
coolant |
:
3 gallons |
| Engine
oil, wet sump option |
:
6 quarts |
| Engine
oil, dry sump option |
:
10 quarts |
| PSRU
oil |
:
2 quarts |
| |
|
| Speeds
|
|
| |
|
| Vx
/ best angle of climb |
:
75 mph |
| Vy
/ best rate of climb |
:
82 mph |
| Vne
/ never exceed speed |
:
340 mph |
| Vc
/ cruise speed @ 3500 rpm / LS2 |
:
225 mph |
| Va
/ maximum maneuvering speed in rough air |
:
230 mph |
| Vno
/ maximum structural cruise speed |
:
270 mph |
| Vso
/ stall speed dirty |
:
59 mph |
| Vs1
/ stall speed clean |
:
74 mph |
| Vlof
/ takeoff speed |
:
75 mph |
| Vle
/ maximum landing extended operating speed |
:
188 mph |
| Vfe
/ maximum flaps extend speed |
:
149 mph |
| Best
glide |
:
79 mph |
| Normal
approach speed |
:
80 - 85 mph |
| Normal
touchdown speed |
:
65 - 70 mph |
| Takeoff
distance to clear 50' obstacle |
:
1000' |
| Landing
distance |
:
1650' |
| Rate
of climb / 4500 rpm |
:
3000+ fpm |
| |
|
| Engine
options |
|
| |
|
| Chevrolet
LS2 (400 cu.in.) power @ takeoff / cruise |
:400
hp / 325 hp |
| Chevrolet
LS7 (427 cu.in.) power @ takeoff / cruise |
:
470 hp / 370 hp |
| |
|
| Propeller
Speed Reduction Unit |
|
| |
|
| 2.26:1 |
standard ratio, 3.000" Hyvo chain |
| 1.86:1 |
optional ratio, 3.000" Hyvo chain |
| Self-contained
lubrication system |
|
| |
|
| Propeller
|
|
| |
|
| MT
Constant Speed, 86.000", composite 4 blade |
|
| |
|
| Endurance
/ Consumption |
|
| |
|
| Fuel
consumption at takeoff power setting / LS2 |
: 20 - 22 gph |
| Fuel
consumption at cruise power setting / LS2 |
:
14 - 15 gph |
| Endurance,
standard tanks |
:
4 hours |
| Endurance,
with drop tanks fitted |
:
5.5 hours |
