Product overview
The United Aircraft T333 rotor system is designed for the T333 unmanned helicopter. It has a rotor diameter of 10.2 m and combines a bearingless hub with an integrated composite flexible beam design. Its control system uses United Aircraft's electrically controlled coaxial rotor technology. United Aircraft has completed the T333 platform's rotor aerodynamic design and related flight-test verification, taking account of the platform's requirements for take-off weight, altitude and flight speed.
Specifications
| Specification | Value & conditions |
|---|---|
| System designation | T333 Rotor SystemNamed system case |
| Hub construction | Bearingless hub with integrated composite flexible beamsT333 unmanned helicopter rotor system |
| Rotor configuration | T333; bearingless hub; 10.2 m rotor diameterT333 unmanned helicopter rotor system with an integrated composite flexible-beam design. |
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