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Mercury HP |
Pegasus HP |
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AMT Netherlands Web Site
(click here)
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Mercury HP |
Pegasus HP |
Olympus |
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Engine diameter. |
100 mm |
3.9 inches |
120 mm |
4.7 inches |
130 mm |
5.1 inches |
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Engine length. |
220 mm |
8.7 inches |
264 mm |
10.4 inches |
270 mm |
10.6 inches |
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Engine weight. |
1400 g |
3.1 Lbs |
2100 g |
4.6 Lbs |
2400 g |
5.3 Lbs |
System airborne
weight.
Engine,ECU,pump,battery,thermosensor,straps. |
2005 g |
4.4 Lbs |
2705 g |
5.9 Lbs |
3100 g |
6.9 Lbs |
Thrust @
S.T.P.*
(*see below)
15 Deg. Celsius
/ 1013 Mbar.
59 Deg. Fahrenheit
/ 29,91 in. |
88 N/9Kg
@ 149,800 |
19,8 Lbf
@ 149,800 |
157 N/16KG
@117,000 |
35,3 Lbf
@ 117,000 |
190 N/19.4KG
@110,000 |
42.7 Lbf
@110,000 |
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Maximum r.p.m. |
153,000 |
120,000 |
112,000 |
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Thrust @ idle r.p.m. |
4 N |
0.9 Lbf |
6 N |
1.3 Lbf |
7 N |
1.5 Lbf |
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Idle r.p.m. |
47,600 |
37,000 |
33,000 |
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Pressure ratio @
max. r.p.m. |
2.8 : 1 |
3.2 : 1 |
4 : 1 |
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Mass flow. |
250 g/sec
@88 N |
0.55 Lb/sec
@19,8 Lbf |
375 g/sec
@157 N |
0.85 Lb/sec
@35,3 Lbf |
400 g/sec
@190 N |
0.95 Lb/sec
@42.7 Lbf |
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Normal Exhaust
GasTemperature. |
650 C |
1200 F |
600 C |
1110 F |
650 C |
1200 F |
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Maximum Exhaust
GasTemperature. |
700 C |
1290 F |
675 C |
1250 F |
700 C |
1290 F |
Fuel Consumption
@ max.
r.p.m. and S.T.P. *
(*see below) |
290 g/min
@88 N |
10 oz/min
@19,8 Lbf |
450 g/min
@157 N |
15.7 oz/min
@35,3 Lbf |
550 g/min
@190 N |
19 oz/min
@42.7 Lbf |
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Fuel types. |
Kerosene - Paraffin
- Jet A1 - White Spirit |
| * S.T.P.
Standard Temp. & Pressure |
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All
specifications are subject to change without notice.
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Suitable oils for our range
of turbines are:
AeroShell 500
(delivered with AMT Netherlands engines)
EXXON 2380
Mobil Jet oil II
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