Powerplant System
The Quantum Turbine Powerplant system for our FLS Microjet was designed around the PBS TJ100 turbojet engine. This compact, lightweight, high-tech engine features a modern FADEC control, and a high thrust to weight ratio. BD-Micro worked directly with PBS to further develop several engine safety features for our application.
ENGINE SPECIFICATIONS
|
Max Thrust |
265 lbs |
|
Min SFC |
1.10 lbs/lbt/hr |
|
Start Time |
< 35 sec` |
|
Acceleration 75% To 95% |
< 10 sec |
|
Oil Consumption |
150 ml/hr. max |
|
Turbine Oil Type |
MIL-L-23699 |
|
Jet Fuel Type |
Jet A, Jet A1, JP4 |
|
Initial Cycle Life |
600 starts |
|
Power Output To Battery |
720 watts (25 a) |
|
Max Re-light Altitude |
26,000 ft |

In developing the Quantum Turbine Powerplant System for the FLS Microjet our primary goals were safety and reliability. To that end, we dedicated extensive resources to design and testing. Several rounds of revision were completed before we were satisfied with the results.
The powerplant system is comprised of several sub-systems in addition to the engine unit. These sub-systems are made up of the following:
1) Mounting and Supports
2) Fuel System
3) Air Induction
ii. FOD screen on engine inlet
4) Electrical Systems
iii. Autonomous engine starting (no external power required)
6) EFIS Display and monitoring of engine parameters
7) Smoke System
8) Thrust Attenuator
9) Performance Optimized Jet Thrust Nozzle
