Atlas/ Glossary/ Takeoff thrust, with respect to turbine engines,

General

Takeoff thrust, with respect to turbine engines,.

Takeoff thrust, with respect to turbine engines,

the jet thrust that is developed under static conditions at a specific altitude and atmospheric temperature under the maximum conditions of rotorshaft rotational speed and gas temperature approved for the normal takeoff, and limited in continuous use to the period of time shown in the approved engine specification.