LASTA TP
LASTA TP turboprop trainer aircraft
A turboprop development of the basic LASTA trainer with a 450 hp (330 kW) engine burning standard JP-1/JET-A1 fuel, adding ejection seats, air conditioning and an oxygen system and optionally increasing ordnance payload from 200 kg to 400 kg.
Enlarge LASTA TP turboprop trainer aircraft
Specification
| Engine | Rolls-Royce M250-B17F turboprop |
|---|---|
| Maximum engine power | 450 hp (330 kW) |
| Fuel | JP-1 / JET-A1 |
| Ejection seats | Zvezda KS-2012B |
| Optional ordnance payload | 400 kg, increased from 200 kg |
| Armament pylons | Two additional wing pylons |
| Performance basis | Aerobatic version at 1250 kg take-off mass |
| Maximum speed | 400 km/h |
| Stall speed | less than 115 km/h |
| Cruise speed | 380 km/h |
| Maximum rate of climb | 13.5 m/s |
| Bank-angle load factor | 3.4 g |
| Flying height | 7500 m |
| Maximum flight duration | more than 4 hours |
| Maximum flying range | 1200 km |
| Landing length | 265 m |
| Take-off length | 575 m |
| Load factors | +6 / -3 g |
All data provided for information purposes; final specification is defined per contract.