Allison J71
The Allison J71 was a single spool turbojet engine, designed and built in the United States. It began development in 1948 as a much modified J35, originally designated J35-A-23.
Allison J71
The Allison J71 was a single spool turbojet engine, designed and built in the United States. It began development in 1948 as a much modified J35, originally designated J35-A-23.
has abstract
Das Allison J71 ist ein Strahl ...... ub von 44,5 kN bei 6100 min-1.
@de
L'Allison J71 era un motore ae ...... any sulla base del motore J35.
@it
L’Allison J71 était un turboré ...... à l'origine désigné J35-A-23.
@fr
The Allison J71 was a single s ...... riginally designated J35-A-23.
@en
Link from a Wikipage to an external page
Wikipage page ID
Wikipage revision ID
743,476,800
combustion
Cannular, 10 chambers
compression
compressor
developed from
first run
Length
lists
*List of aircraft engines
major applications
manufacturer
related
thrust
type
Afterburning turbojet
weight
hypernym
type
comment
Das Allison J71 ist ein Strahl ...... son als „cannular“ bezeichnet.
@de
L'Allison J71 era un motore ae ...... any sulla base del motore J35.
@it
L’Allison J71 était un turboré ...... à l'origine désigné J35-A-23.
@fr
The Allison J71 was a single s ...... riginally designated J35-A-23.
@en
label
Allison J71
@de
Allison J71
@en
Allison J71
@fr
Allison J71
@it