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Volume 41, Issue 4
1 April 1969
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 41, Issue 4
Review Article| April 01 1969

Powerplant: A brief description of the Spey 512 and RB.162 booster Available to Purchase

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1969
Aircraft Engineering (1969) 41 (4): 24–28.
https://doi.org/10.1108/eb034493

THE Trident 2E is fitted with a further development of the Rolls‐Royce Spey RB.163–25 turbofan engine, designated the Spey 25 Mk. 512–5W. This engine develops a nominal 12,000 lb. take‐off thrust for a dry weight of 2,590 lb.

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© MCB UP Limited
1969
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Suggested Reading

Powerplant: A brief description of the Spey Mk. 512 and the RB.162 booster engine
Aircraft Engineering (February,1971)
The Rolls‐Royce Spey Junior Powerplant
Aircraft Engineering (June,1967)
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Rolls‐Royce Spey Power Plant: Brief Details of the Engine Design and Testing Programme
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Hawker Siddeley Trident 2E: The background to the development of the Trident and a brief introduction to the 3B
Aircraft Engineering (April,1969)

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