A SUMMARY OF OPERATING CONDITIONSnEXPERIENCED BY THREE MILITARY HELICOPTERS AND AnMOUNTAIN-BASED COMMERCIAL HELICOPTER

摘要

The results of a survey of the flight conditions experienced by three military helicopters engaged in simulated and actual military missions, and a commercial helicopter operated in the mountainous terrain surrounding Denver, Colo., are presented. The data, obtained with NASA helicopter VGHN recorders, represent 813 flights or 359 flying hours, and are compared where applicable to previous survey results.nThe current survey results show that none of the helicopters exceeded the maximum design airspeed. One military helicopter, used for instrument flight training, never exceeded 70 percent of its maximum design airspeed.nThe rates of climb and descent utilized by the IFR training helicopter and of the mountain-based helicopter were generally narrowly distributed within all the airspeed ranges. The number of landings per hour for all four of the helicopters ranged from 1.6 to 3.3.nThe turbine-engine helicopter experienced more frequent normal-acceleration increments above a threshold of ±0.4g (where g is accelera¬tion due to gravity) than the mountain-based helicopter, but the mountain-based helicopter experienced acceleration increments of greater magnitude.nLimited rotor rotational speed time histories showed that all the helicopters were operated at normal rotor speeds during all flight conditions.