JetBeetle Tarantula H90
| Tarantula H90 | |
|---|---|
 | |
| JetBeetle Tarantula H90 engine on a Monnett Monerai | |
| Role | Small gas turbine |
| National origin | United States |
| Manufacturer | JetBeetle |
|
| |
The JetBeetle Tarantula H90 is an American gas-turbine engine for use on Homebuilt aircraft
It is capable of producing 90 lbf (0.40 kN) thrust at 88,000rpm.[1][2]
Variants
- Tarantula H90
- 90 lbf (0.40 kN)
JetBeetle Locust H150R
- Locust H150R
- 170 lbf (0.76 kN)
JetBeetle Mantis H250
- Mantis H250
- 250 lbf (1.11 kN)
Applications
Specifications (Tarantula H90)
Data from JetBeetle[3]
General characteristics
- Type: Turbojet
- Length: 18.7 in (470 mm) with starter
- Diameter: 6.5 in (170 mm)
- Dry weight: 16.5 lb (7.5 kg) with starter
Components
- Compressor: single stage centrifugal
- Combustors: Annular combustion chamber
- Turbine: single stage axial
- Fuel type: Kerosene
Performance
- Maximum thrust: 85 lbf (0.38 kN) max continuous
- Thrust-to-weight ratio: 5
Notes
- ↑ "Jetbeetle H90". Retrieved 18 August 2014.
- ↑ "What is the H160 Jetbeetle". Retrieved 14 August 2014.
- ↑ "Products - 2012". jetbeetle.com. Retrieved 19 August 2014.
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