PBS AEROSPACE TJ100

General Specs (cont.)

Detailed Description

The PBS TJ100 is a 4th-GENERATION turbojet engine. The PBS TJ100 is especially suitable for manned and unmanned vehicles. 
These engines are also ideal for gliders and light sports and experimental airplanes. The PBS TJ100 engine is of a compact design and has an excellent power-to-weight ratio of up to 281 lbf with low fuel consumption for its output category. This engine is also suitable for landing on water.

Main features
Compact design, excellent thrust-to-weight ratio and low fuel consumption for its category.
The integrated starter-generator ensures reliable 24V battery start-up, supplies electricity to the vehicle's onboard wiring and cools the engine after shutdown.
Classic design - radial compressor and annular combustion chamber, axial turbine and fixed output nozzle.
Standard equipment fuel-oil system, control system, ignition unit, connection cables and manual or fully automatic control.

Fuel
JET-A, JET-A1, JP4, JP8, TS-1, T2, RT

Lubrication
according to MIL-L-23699 (Mobil Jet oil II, AEROSHELL 560)

Parameters
Thrust: take-off (max. 5 min.) - 281 lbf
Eelctric power output	650 W
Specific fuel consumption at max. thrust - ≤ 1.1376 lb/lbf/hr
Outside diameter - 10.71 in
Engine length	- 25.04 in
Engine weight - 38.80 lb
Max. operating altitude - 32,808 ft
Max. starting altitude - 19,685 ft
Flight speed range - 0 to 0.9 M
Speed range for startup - 0 to 0.6 M

Bought by a previous owner and never used. Comes in sealed and in its original packaging.