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PERFORMANCE
COMPARISON
CHART
|
|
|
Viper
6011
|
Viper
5401
|
L-29
|
L-39
|
ALPHA JET
|
A-10
|
|
Thrust/Empty wt
|
.75
|
.67
|
.39
|
.54
|
.76
|
.83
|
|
T.O. Dist/50ft.
|
800
|
900
|
2800
|
3000
|
3400
|
N/A
|
|
Climb to 10,000 ft min
|
<1.5
|
<2.0
|
5.0
|
3.5
|
2.0
|
2.2
|
|
Max Speed @ 18,000 ft (kts)
|
440
|
440
|
320
|
370
|
535
|
450
|
|
Service Ceiling (feet)
|
45,000+
|
45,000+
|
27,000
|
33,000
|
48,000
|
N/A
|
|
Wing Loading (lb./sqft.
|
23
|
23
|
23
|
36
|
42
|
43
|
|
Sustained G @ 10,000 ft
|
6.2
|
5.5
|
2.3
|
2.2
|
3.2
|
4.0
|
|
Thrust (lb,)
|
3,375
|
3,340
|
1,960
|
3,972
|
5,950
|
18,130
|
|
Empty Wt. Clean
|
5,000
|
5,000
|
5,000
|
7,400
|
7,870
|
21,540
|
|
Cruise (kts)
|
300
|
300
|
235
|
260
|
320
|
300
|
|
Gal/Hr. @ Cruise
|
150
|
145
|
130
|
130
|
270
|
N/A
|
|
Range @ 18,000 ft.
|
420
|
420
|
300
|
500
|
500
|
N/A
|
|
Range w/ wet wings
|
650
|
6502
|
500
|
---
|
---
|
---
|
|
Purchase Cost
|
$140,000
|
$125,000
|
$50,000
|
$275,000
|
$600,000
|
N/A
|
|
|
|
| |
1 Based on limited flight test data
2 Ask about the Vipers' 104 gallon wet wing modification designed and installed by Aero Enterprises.
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