General and specific turbojet design considerations for application in pure hoverjet aircraft; attempt made to establish overall power plant requirements, to define desirable characteristics and to indicate approaches toward improvement of engine specific weight through component design; factors required in maximizing transport range/payload performance are minimum overall to gross weight ratio, minimum hover time, and minimum life engine specific weight.
Turbojet lift engine design for VTOL transports
Can Aeronautical J
Canadian Aeronautical Journal ; 5 , n 6
1959
9 pages
Aufsatz (Zeitschrift)
Englisch
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Turbojet Lift Engine Design for VTOL Transports
NTRS | 1958
|Engineering Index Backfile | 1956