To Non-Java ALLSTAR Network Website
Please let me remind all of you--this
material is copyrighted. Though partially funded by NASA, it is still a
private site. Therefore, before using our materials in any form, electronic or
otherwise, you need to ask permission.
There are two ways to browse the site: (1) use the search button above to find specific materials using keywords; or,
(2) go to specific headings like history, principles or careers at specific levels above and click on the button.
Teachers may go directly to the Teachers' Guide from the For Teachers button above or site browse as in (1) and (2).
Pratt & Whitney Engines
F100-PW-229 TURBOFAN ENGINE
Aircraft used on (click here)
|Maximum Thrust (Full Augmentation)||29,100 lb (129.4 kN)|
|Intermediate Thrust (Nonaugmented)||17,800 Ib (79.2 kN)|
|Weight (Specification Maximum)||3,740 lb (1,681 kg)|
|Length||191 in. (4.85 m)|
|Inlet Diameter||34.8 in. (0.88 m)|
|Maximum Diameter||46.5 in. (1. 18 in)|
|Overall Pressure Ratio||32 to 1|
This material is copyrighted to Pratt and Whitney and they retain and reserve all rights to this material. The use of this material by the ALLSTAR network is with permission of Pratt and Whitney. The ALLSTAR network's copyright applies to the format used in presenting this material. Pratt and Whitney should be contacted directly for permission to use this material.
Send all comments to firstname.lastname@example.org
© 1995-2017 ALLSTAR Network. All rights reserved worldwide.
|Funded in part by||Used with permission from Pratt & Whitney|
Updated: March 12, 2004