Product Updates
10/13/2006
Bob Wilcox
Attention Kero Start Engines Users:
If the engine fails to start, you can get excess kerosene in the engine. YOU CANNOT REMOVE EXCESS KEROSENE BY TILTING THE PLANE WITH THE NOSE UP IN THE AIR.
(read more)
9/25/2006
Failsafe and the Auxiliary channel:
DO NOT ASSUME THAT YOU PROGRAM THE AUXILIARY CHANNEL LIKE THE THROTTLE CHANNEL FOR FAILSAFE!
(read more)
01/31/2006
When installing the Kerosene
starter in the P60, please note:
The P60 glow plug boss may
have damaged threads near the combustion chamber.
(read more)
12/19/2005
A new version for Jettronic for Windows is available. Check out downloads for the latest version.
JetCat USA News
9/27/2007
At
Florida Jets 2007, JetCat USA
introduced the Titan SE and P-120 SE
turbines. These new Special Edition
turbines feature revolutionary
technology allowing them to
accelerate rapidly while maintaining
the legendary JetCat reliability.
1/3/2005
This is an e-mail from one of our long time customers, Rick Silz. Rick flies at Rabbit Dry Lake here in S. California. This guy really flies!!!
(read more)
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JetCat P-70 turbine complete with starter includes:
- Jet-tronic ECU (fuel control electronics)
- GSU (Display and Programmer)
- LED I/O board
- Miniature fuel pump
- Electronic starting gas valve
- Electronic Fuel valve
- Fuel tubing, tubing connector set, filters, and cable set
- 2 cell, 2500mA LiPoly battery pack
- Starting gas tank
- Turbine mounting clamp, RamTec compatible
- Detailed instruction manual
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Thrust: |
17.5 LB @ 123,000 RPM
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Weight: |
2.6 LB, incl. starter
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Diameter: |
3.7 inches
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RPM Range: |
35,000 - 123,000
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Exhaust gas temp.: |
620°C
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Fuel consumption: |
8 oz per/min at full power
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Fuel: |
Jet A1, 1-K kerosene
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Lubrication: |
approximately 5% synthetic turbine oil in the fuel
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Maintenance interval: |
25 hours
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P70 Thrust Chart
| RPM |
Thrust |
| 38,000 |
0.75 |
| 93,000 |
8.0 |
| 101,000 |
10.0 |
| 107,000 |
12.0 |
| 113,000 |
14.0 |
| 118,000 |
16.0 |
| 123,000 |
17.5 |
The values are approximate and can vary slightly from engine to engine.
Values at Standard Temperature and Pressure.
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