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TJ80 TURBOJET ENGINE

TJ80 TURBOJET ENGINE

Product catalog summary

Overview: The TJ80 is a small turbojet engine designed for use in missiles, target drones, and UAVs. It is manufactured by Prvni brnenska strojirna Velka Bites, a.s., located in the Czech Republic.

Technical Specifications:

Max Thrust: 900 N for 5 minutes at 100% mode.
Continuous Thrust: 800 N at 97% mode.
Specific Fuel Consumption (SFC): 0.122 kg/N/h at 100% mode.
RPM: 58,000 RPM at 100% mode.
Airflow: 1.47 kg/sec at 100% mode.
Compression Ratio: 4.7.

Operational Conditions:

Starting Envelope: Altitude 0 to 6,000 m; Ambient temperature -40°C to +50°C; Speed < 0.6 M.
Flight Envelope: Altitude 0 to 10,000 m; Ambient temperature -50°C to +50°C; Speed < 0.9 M.

Additional Data:

Electric Generator Power: 28 V - 1,000 W.
Engine Starting: BLDC starter.
Standard Accessories: Engine control unit (ECU), Exciter ignition, Electromagnetic stop valve.
Fuel: JET-A1, TS-1, RT.
Lubrication: 3% oil in fuel (MIL-L-23 699).

Dimensions and Weight:

Max Outer Diameter: 235 mm.
Length: 512 mm (including starter-generator).
Weight: 10.5 kg.

Main Features:

Compact design.
Excellent weight/thrust ratio.
Low fuel consumption in the given output category.
Uniform fuel for both the engine and lubrication.
Maintenance-free operation.
Electric start with the possibility of in-flight restart.
Integral generator and inverter.
Startability at high altitude and high speed.

Contact Information: Sales Department, Prvni brnenska strojirna Velka Bites, a.s., Vlkovska 279, 595 01 Velka Bites, Czech Republic. Tel: +420 566 822 304, Fax: +420 566 822 372, E-mail: [email protected], Website: www.pbsvb.com

Catalog excerpts

Small turbojet engine designed for missiles, target drones and UAVs

Open the catalog to page 1

Technical parameters Max. thrust (5 min.) Thrust (continuous) Specific fuel consumption (SFC) RPM Airflow Compression ratio Operation conditions: Altitude Ambient temperature Speed Additional data: Electric generator power Engine atarting Standard accessories (airframe installation) Fuel Lubrication Mode 100% 97% 100% 100% 100% Ink] Starting envelope 0 e 6,000 m -40°C e +50°C < 0.6 M 28 V - 1,000 W BLDC starter Engine control unit (ECU), Exciter ignition, Electromagnetic stop valve JET-A1, TS-1, RT 3% oil in fuel (MIL-L-23 699) Dimension and weight: Max. outer diameter 235 mm Length (including...

Open the catalog to page 2

TJ80 TURBOJET ENGINE

TJ80 TURBOJET ENGINE

Catalog excerpts

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