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PBS Turbojet engine TJ150

PBS Turbojet engine TJ150

PBS Turbojet engine TJ150

Product catalog summary
Main Features:
  • Compact design with excellent thrust-to-weight ratio.
  • Low fuel consumption for its power category.
  • Equipped with an electric starting system and integrated starter-generator.
  • Capable of water landing and both ground and in-flight restarts.
  • Customizable variations available upon request.
Technical Parameters:
  • Max thrust: 1,500 N.
  • Power supply: 28 V DC with 600 W electrical power output.
  • Specific fuel consumption: 0.119 kg/N/h.
  • Dimensions: 272 mm diameter, 520 mm length.
  • Weight: 19.6 kg (43.2 lb) with accessories weighing 2.2 kg (1 kg).
  • Max engine speed: 55,300 RPM.
  • Fuel types: JET A, A-1, B (DERD 2494), TS-1, T2, RT (GOST 10227-86).
  • Oil: Mobil Jet Oil II / AEROSHELL 560 (MIL-L-23699).
Operating Range:
  • Engine operation altitude: 0 to 9,000 m (0 to 29,528 ft).
  • Speed: 0 to 0.9 Mach.
  • Ambient temperature: -50 °C to +45 °C (-58 °F to +113 °F).
  • Engine start altitude: 0 to 4,000 m (0 to 13,123 ft).
  • Speed: 0 to 0.4 Mach.
  • Ambient temperature: -30 °C to +45 °C (-22 °F to +113 °F).
Accessories:
  • Standard assembly includes internal fuel-oil system, control system (FADEC), ignition unit, and interconnecting cable.
  • Optional accessories include electromagnetic fuel valve, fuel filter, control lever, signalling panel, boost pump, reduction valve, interface CAN, user software, and front and exhaust cover.
Contact Information:
  • PBS Velka Bites, a. s., Vlkovska 279, 595 01 Velka Bites, Czech Republic, EU.
  • Sales Department: Tel.: +420 566 822 304, E-mail: [email protected], Website: www.pbsvb.com
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Catalog excerpts

PBS Turbojet engine TJ150-1

TJ150 TURBOJET ENGINE Designed for UAVs, Target Drones and Missiles

 Open the catalog to page 1
PBS Turbojet engine TJ150-2

• Compact design • Excellent thrust-to-weight ratio • Low fuel consumption at its power category • Electric starting system • Integrated starter-generator • Suitable for water landing • Possibility of ground and in-flight restart • Variations according to customer's request Standard assembly: - Internal fuel-oil system - Control system (FADEC) - Ignition unit - Interconnecting cable Optional accessories: - Electromagnetic fuel valve - Fuel filter - Control lever - Signalling panel - Boost pump - Reduction valve - Interface CAN - User software - Front and exhaust cover Operating range - engine...

 Open the catalog to page 2
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.