Category Frank N. Piasecki Achievements

PA-4

With the advent of nuclear submarines, U.S. Navy efforts to base helicopters aboard destroyers as a weapon delivery system increased. Limitations of storage space gave impetus to a drone concept. Piasecki proposed such a concept – the “SeaBat” – specifically…

PA-2C

The PA-2C was designed to be a vertical take-off aircraft capable of sustained, high-speed level flight (operating from aircraft carriers, cruisers, destroyers, and unprepared landing sites). Called the “RingWing”, it combined two ducted propellers that contained an integrated system of…

HRP-2

The HRP-2, an improved version of the HRP-1 “Rescuer”, with an aerodynamically streamlined all-metal fuselage, was developed for the assault mission of the U.S. Marine Corps. In the earlier tandems, the long distance from the cockpit to the landing gear…

HRP-1

The concept of a flying mock-up permitted a rapid demonstration of the unique configuration and a measurement of the XHRP-X flight and control characteristics. Early design improvements in the XHRP-1 prototype resulted. Mission Transport, Crane, Tow, ASW Crew 2 Passengers…

H-21

The H-21 used the same basic configuration as the HRP-2. The 41 foot rotor was increased to 44 feet, and a 1,425 horsepower engine installed, increasing the gross weight from 7,255 to 14,700 lbs. The H-21A was the winner of…

16H-3

Weight and Performance Summary: (2) UCAL Turbines at 750 shp each Characteristics VTO (lb) STO (lb)*** Weights 10,440 10,700 Design Gross Weight 5,995 5,995 Empty Weight 4,445 4,745 Payload (plus 1 pilot) with 2,118 lb fuel and oil (full tanks)*…

16H-1A Pathfinder II

In 1964, under Army contract, PiAC modified the Pathfinder (16H-1) to attain speeds over 200 mph. A G.E. T-58 shaft-turbine rated at 1,050 shp, a new drive system, a new propeller to absorb the increased power and a 44 foot…

16H-1 Pathfinder

A comprehensive market survey of the transportation needs both in the helicopter market and the short haul airplane market, revealed a large percentage of potential short haul operations that were limited by available airports and surface distances to their end…