File:Pratt and Whitney TF30-P-109 (9694469193).jpg

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English: Maximum thrust: 14,560 lbf (64.766kN), 25,100 lbf (111.65kN) with afterburning. Overall pressure ratio: 19.8. Bypass ratio: 0.878:1. Turbine inlet temperature: 2150F (1176C). Thrust-to-weight ratio: 6.0 - Day 2 Defence Force Air Show 4-5 October 2008. File: Pratt_&_Whitney_TF30-P-109_YAMB_20081005_3628
Set: Defence Force Air Show RAAF Amberley 4-5 October 2008
Tags: A8; YAMB; 2008; Defence Force Air Show 2008; RAAF; F111; Nikon D70; RAAF Serials Numbers - Series 3; General Dynamics
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Source https://www.flickr.com/photos/robertfrola/9694469193/
Author Robert Frola
Camera location27° 38′ 24.43″ S, 152° 42′ 42.19″ E Kartographer map based on OpenStreetMap.View this and other nearby images on: OpenStreetMapinfo

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This file comes from the Robert Frola collection and is copyrighted.
Note: This permission only extends to photos taken by Robert Frola at this link, this link, and this link, in addition to files which may be provided via email. It does not include any other content from the above sites which has not been provided by Robert Frola.
GNU head Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License.
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Date/TimeThumbnailDimensionsUserComment
current13:47, 25 April 2014Thumbnail for version as of 13:47, 25 April 20141,600 × 1,063 (1.36 MB)Fæ (talk | contribs)== {{int:filedesc}} == {{information |description={{en|1=Maximum thrust: 14,560 lbf (64.766kN), 25,100 lbf (111.65kN) with afterburning. Overall pressure ratio: 19.8. Bypass ratio: 0.878:1. Turbine inlet temperature: 2150F (1176C). Thrust-to-weight rat...

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