Description and operating notes relating to the N.A.E. reheated Orenda L. engine installed in an F-86 Sabre Air® AFT

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DOI	Resolve DOI: https://doi.org/10.4224/40003862
Author	Search for: Levy, G. G.¹; Search for: Fowler, H. S.¹; Search for: Millar, D. A. J.¹
Affiliation	National Research Council Canada. National Aeronautical Establishment
Format	Text, Memorandum
Physical description	9 p.
Abstract	The following notes describe the N.A.E. reheat system as applied to an Orenda II4,engine installed in P-86 Sabre aircraft No. 23544. The description, and some operating notes, are written mainly for the benefit of pilots and technical personnel who will be concerned with the operation of this aircraft. Basically, the layout of the reheat system is similar to that used on the Derwent Meteor aircraft. Information on this installation, together with notes outlining the reheat principle, may be found in Ref. 1.
Publication date	1956-03-20
Publisher	National Research Council Canada
Series	Laboratory Memorandum (National Research Council Canada. National Aeronautical Establishment. Engine Laboratory), no. NAE-ENG-38 (20 March 1956).
Language	English
Peer reviewed	No
Identifier	NAE-298
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Record identifier	b8e1abc8-8ef9-4381-8082-859b4cbf2305
Record created	2025-11-12
Record modified	2025-11-27