2011Journal of AircraftRequires access

Safety Considerations for Helicopter Roll On Takeoffs

K. Enciu, Alon Rosen

Open publisher page 3 citations

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.

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What this paper is about

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.

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Available 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.

Key concepts: Takeoff, Runway, Airspeed, Takeoff and landing, Aeronautics, Engineering, Engine power, Aerospace engineering

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