 |
Mercury HP |
|
Olympus HP | Titan UAV | ||||
|---|---|---|---|---|---|---|---|---|
| Engine diameter. | 100 mm | 3.9 inches | 120 mm | 4.7 inches | 130 mm | 5.1 inches | 147 mm | 5.8 inches |
| Engine length. (Airstart engine) | 220 mm | 8.7 inches | 264 mm | 10.4 inches | 267 mm | 10.5 inches | 268 mm | 10.5 inches |
| Engine length. (Electric start engine) | 292 mm | 11.5 inches | 342 mm | 13.4 inches | 374 mm | 4.7 inches | 385 mm | 15.1 inches |
| Engine weight. (Airstart engine) | 1400 g | 3.1 Lbs | 2125 g | 4.6 Lbs | 2475 g | 5.4 Lbs | 2975 g | 6.6 Lbs |
| Engine weight. (Electric start engine) | 1550 g | 3.4 Lbs | 2255 g | 4.9 Lbs | 2850 g | 6.3 Lbs | 3350 g | 7.4 Lbs |
| System
airborne weight. (Air start system)
Engine,ECU,pump,battery,thermosensor,straps. |
2005 g | 4.4 Lbs | 2705 g | 5.9 Lbs | 3150 g | 6.9 Lbs | 4200 g | 9.3 Lbs |
| System
airborne weight. (E-start system)
Engine,ECU,pump,battery,thermosensor,straps. |
2235 g | 5.1 Lbs | 3075 g | 6.75 Lbs | 3795 g | 8.35 Lbs | 4575 g | 10 Lbs |
| Thrust
@ S.T.P.*
(*see
below)
15 Deg. Celsius / 1013 Mbar. 59 Deg. Fahrenheit / 29,91 in. |
88N
/ 9Kp
@ 151,200 |
19,8
Lbf
@ 151,200 |
167N
/ 17,0Kp
@119,500 |
37,5
Lbf
@ 119,500 |
230N
/ 23.5Kp
@108,500 |
51.7
Lbf
@108,500 |
392N
/ 40Kp
@95,000 |
88,2
Lbf
@95,000 |
| Maximum allowed r.p.m. | 151,900 | 120,000 | 112,000 | 97,000 | ||||
| Thrust @ idle rpm | 4 N | 0.9 Lbf | 6 N | 1.3 Lbf | 8 N | 1.8 Lbf | 13 N | 2.9 Lbf |
| Idle rpm | 47,600 | 37,000 | 36,000 | 30,000 | ||||
| Pressure ratio @ max. rpm | 2.8 : 1 | 3.2 : 1 | 3.8 : 1 | 3.8 : 1 | ||||
| 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 |
450
g/sec
@230 N |
0.99
Lb/sec
@51.7 Lbf |
660
g/sec
@392 N |
1.46
Lb/sec
@82.2 Lbf |
| Normal Exhaust GasTemperature. | 650 C | 1200 F | 600 C | 1110 F | 700 C | 1290 F | 700 C | 1290 F |
| Maximum Exhaust GasTemperature. | 750 C | 1380 F | 675 C | 1250 F | 750 C | 1380 F | 750 C | 1380 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 |
640
g/min
@230 N |
22.5
oz/min
@51.7 Lbf |
1120g/min
@392 N |
39.5
oz/min
@88.2 Lbf |
| Fuel types. | Kerosene - Paraffin - Jet A1 - White Spirit | |||||||
| *
S.T.P. Standard Temp. & Pressure
Temp: 15 Degrees Celcius / 59 Degrees Fahrenheit Pressure: 1013 Mbar / 29.91 in |
||||||||
| All specifications are subject to change without notice. | ||||||||
| Suitable oils for our range of turbines are: | AeroShell
500
AeroShell 560 Mobil Jet oil II |
|||||||