Safety Considerations for Helicopter Roll On Takeoffs
K. Enciu, Alon Rosen
Abstract
K. Enciu, Alon Rosen
Abstract
A six-degree-of-freedom simulation of helicopter roll on takeoff is used for evaluation of a twin-engine helicopter continued takeoff trajectory, following one engine failure. For this study, an AH-64A Apache was used. The simulation is used for the determination of the required runway length that will enable safe continued takeoff using the remaining engine’s power.Apreliminary optimizationwas carried out for thedefinition of the liftoff airspeed and critical decision point height that minimize the required runway length.
OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
A six-degree-of-freedom simulation of helicopter roll on takeoff is used for evaluation of a twin-engine helicopter continued takeoff trajectory, following one engine failure. For this study, an AH-64A Apache was used. The simulation is used for the determination of the required runway length that will enable safe continued takeoff using the remaining engine’s power.Apreliminary optimizationwas carried out for thedefinition of the liftoff airspeed and critical decision point height that minimize the required runway length.
Key concepts: Takeoff, Runway, Airspeed, Takeoff and landing, Aeronautics, Engineering, Engine power, Aerospace engineering