R-4

🇺🇸United States
Sikorsky
1944 – Present
Overview
R-4
The Sikorsky R-4, developed from the VS-300 and first flown in January 1942, was a pioneering helicopter that set multiple records in endurance, altitude, and speed. Designed with a three-bladed rotor and powered by a radial engine, it was primarily used for transport and medical evacuation, lacking significant armament capabilities.
Specifications

General

Crew1
Max Speed Kmh121 km/h
Weight Max Kg1,150 kg
Service Ceiling M2,400 m
Research Notes

Development Context

R-4 is best understood as a early production military helicopter, rather than as a bare specification line. The Sikorsky R-4 was the first production helicopter and gave the U.S. military an early practical rotorcraft for rescue, liaison, and experimental utility missions. This richer context connects the equipment’s specifications to doctrine, industrial constraints, and operational use.

Design and Tradeoffs

The design choices behind R-4 show the tradeoffs that shaped its battlefield role. Its piston engine, single main rotor, tail rotor, and small payload were primitive by later standards, but they proved that vertical-lift aircraft could perform missions fixed-wing aircraft could not. This richer context connects the equipment’s specifications to doctrine, industrial constraints, and operational use.

Service and Legacy

The service record of R-4 explains why the equipment remains historically useful to compare. The R-4’s value lies in opening the military helicopter era, especially for rescue and evacuation roles that became central in later conflicts. This richer context connects the equipment’s specifications to doctrine, industrial constraints, and operational use.

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