Development of Thrust Augmentation Technology for the Pegasus Vectored Thrust Engine

821390

02/01/1982

Event
Aerospace Congress and Exposition
Authors Abstract
Content
Front nozzle thrust augmentation, on lift/cruise engines like the Pegasus, could greatly improve the range and load carrying capacity of Harrier/AV-8B type VTOL aircraft and is essential for supersonic derivations. However its introduction requires several new technologies to be developed for the augmentor itself, for the augmentor and engine control system and to cater for various potentially adverse ground effects and related matters. These are the subject of a number of current research and development programmes which will lead to an engine demonstration of an advanced augmentor.
Meta TagsDetails
DOI
https://doi.org/10.4271/821390
Pages
12
Citation
Sotheran, A., "Development of Thrust Augmentation Technology for the Pegasus Vectored Thrust Engine," SAE Technical Paper 821390, 1982, https://doi.org/10.4271/821390.
Additional Details
Publisher
Published
Feb 1, 1982
Product Code
821390
Content Type
Technical Paper
Language
English