Many factors,such as deck motion and air wave,influence the determination of the approach speed which has an important effect on landing safety. Until recently,there are no design criteria about approach speed of carrier aircraft in the current standards and available publications. Therefore,the requirements of stall margin, longitudinal acceleration ability,altitude correction and field-of-view on approach speed were researched. Based on the flight dynamics model,the flight simulations were conducted to study the effect of the response time of engine,wave off requirements,elevator efficiency and deflection rate on the approach speed. The results presented that the approach longitudinal acceleration and altitude correction ability had crucial influence on the approach speed envelope of the aircraft. The limitations of the control requirements,field- of- view requirements and gear were also given through the simulation and analysis. Based on the above results,the approach speed envelope were determined. Many factors, such as as deck motion and air wave, influence the determination of the approach speed which has an important effect on landing safety. , the requirements of stall margin, longitudinal acceleration ability, altitude correction and field-of-view on approach flight were researched. Based on the flight dynamics model, the flight simulations were conducted to study the effect of the response time of engine, wave off requirements, elevator efficiency and deflection rate on the approach speed. The limitations presented the control requirements, field-of-view requirements and gear was also given through the simulation and analysis. Based on the above results, the approach speed envelope were determined.