This document provides a general comparison of the state of the art of Soviet helicopter design vs. that of the West (U.S. in particular). It includes both commonalities and differences in conceptual design philosophies by addressing design parameters and design effectiveness according to accepted criteria. The baseline for comparison is by design gross weight which is presented in four categories: under 12,000 lb, 30-100,000 lb, and greater than 100,000 lb.
A comparative study of Soviet versus Western helicopters. Part 1: General comparison of designs
1983-03-01
Report
Keine Angabe
Englisch
NTIS | 1969
Engineering Index Backfile | 1959
Engineering Index Backfile | 1957