STRAERO S.A.

STRAERO - over 25 years of validation & certification tests for aircraft structures

STRUCTURAL CERTIFICATION
for all Romanian aircraft: IAR-93 jet fighter, IAR-99 jet trainer, IAR-823 propeller trainer, IAR-827, AG-6, IAR-35 and IS-28D2

STRUCTURAL CERTIFICATION
for IAK-52 trainer, produced under licence

STATIC AND FATIGUE CERTIFICATION
tests for IAR-330H and IAR-330H SOCAT improved helicopters

VIBRATION TESTS
for various subassemblies as parts of manufacturing Rolls-Royce Viper and Spey engines

SEISMIC QUALIFICATION TESTS
for equipment used in nuclear power plants

VARIOUS TESTS
under static, dynamic, vibration, fatigue and other loadings for industrial equipment

Helicopter blade aero-elastic analysis for IAR330 PUMA helicopter

Elasto-plastic domain behaviors for IAR330 PUMA helicopter

Designing & conducting specific tests for composite materials testing procedures, stability studies using EFM, shock and torsion behavior and shock waves behavior in glass fiber composites,

In flight flutter and vibrations tests for IAR-35, IAR-46 general aircarft and IAR-93 jet fighter

Fatigue loads measurement for IAR-823 propeller trainer, IAR-827 and IAR-99 jet trainer

Aero-servo-elastic domain behaviors for IAR-93 jet fighter

Nonlinear structural dynamics for IAR-330 PUMA SOCAT enhanced helicopter and GALAXY israelian transport aircraft - local computing using NASTRAN

Dynamic analysis of aircraft with external stores for IAR-330 PUMA SOCAT enhanced helicopter

Software development: Data Acquisition & Processing for Dynamic Parameter Computation Software Kit, Structure Displacement Computing & Visualization Software, Data Acquisition & Processing for Pulse and Noise Signals Software, Time Processing Software for Acquired Data, Software for Sinus Scanning Simulation

On – going projects

o Low – weight pipes with honey – comb structure

o Multi-layers materials with direct adhesion

o Design and manufacture of endurance testing installation for DACIA – RENAULT component car

o Vibration attenuation of flat structure by rheological dumping systems

Glassfibre ultralight remote controlled aircraft [ UAV ], designed for different missions such as:

o reconnaissance flights above ground
o antiaircraft auxiliary target
o technical target on radiolocator
o monitoring flights using cameras for photographic reconnaissance

Dimensions, external

Wing span 4.0 m
Length, overall 2.2 m
Height, overall 0.7 m

Weights

Empty, equipped 27.5 Kg
Max. T-O weight 40 Kg
Fuel weight 3.5 Kg

Capacities

Fuel consumption 3.5 l/h
Useful weight 12.5 Kg

Performances

Max. speed 140 Km/h
Cruising speed 125 Km/h
Limit speed 60 Km/h
T - O run 35 m
Rate of climb 6.7 m/s
Autonomy (standard tank) 1.5 h
Max. ceiling 2000 m
Radius of action :
- by radiolocator 50 Km
- at view 5 Km

Optional equipment

warping device
control column
parachutes launcher
auxiliary tank