Study investigates whether military and commercial transport capabilities of helicopter are likely to be surpassed in future by different VTOL designs and is confined to performance capabilities and cost of medium size, unpressurized, low subsonic speed, cargo, or passenger carrying vehicles; propulsion systems; VTOL, STOL and ejector configurations tabulated; method of analysis and ground rules; military and commercial direct operating costs, military and commercial capability.
V/STOL cargo airplane characteristics
Aerospace Eng
Aerospace Engineering ; 20 , n 1
1961
5 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
STOL demonstrated feasible for large cargo BLC airplane
Engineering Index Backfile | 1961
|Engineering Index Backfile | 1960
|Preliminary design of "ARAVA" STOL airplane
Engineering Index Backfile | 1967
|Commercial STOL - The Airplane, the Airport
SAE Technical Papers | 1978
|Fan inlet for a V/STOL airplane
NTRS | 1977
|