Two basic versions to be made available; helicopter version, designated LTC1B-1, has nominal output shaft speed of 6000 rpm; for fixed wing applications Model LTC1D-1 is being developed.
Lycoming T53
Flight
Flight ; 69 , n 2466
1956
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1938
Engineering Index Backfile | 1963
Engineering Index Backfile | 1938
Tema Archive | 1996
|Engineering Index Backfile | 1938