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F135

F135

F135

Product catalog summary
Product Overview:
The F135 engine is a dependable fifth-generation power source designed for both land and sea applications, specifically for the F-35B Short Takeoff and Vertical Landing (STOVL) aircraft. It is renowned for its single-engine reliability and affordability, leveraging proven technologies from fifth-generation fighter jets.
Engine Characteristics:
  • Maximum thrust class: 41,000 pounds (182.4 kN)
  • Intermediate thrust class: 27,000 pounds (120.1 kN)
  • Short takeoff thrust class: 40,740 pounds (181.2 kN)
  • Hover thrust class: 40,650 pounds (180.8 kN)
  • Main engine thrust: 18,680 pounds (83.1 kN)
  • Lift fan thrust: 18,680 pounds (83.1 kN)
  • Roll post thrust: 3,290 pounds (14.6 kN)
  • Engine length: 369 inches (9.37 m)
  • Main engine inlet diameter: 43 inches (1.09 m)
  • Main engine max diameter: 46 inches (1.17 m)
  • Lift fan inlet diameter: 51 inches (1.30 m)
  • Lift fan max diameter: 53 inches (1.34 m)
Key Features:
  • Advanced health monitoring and network logistics support to reduce sustainment costs and increase mission readiness.
  • Enables unmatched stealth combat capabilities and effectiveness.
  • Incorporates the Rolls-Royce LiftFan®, Driveshaft, 3 Bearing, and Roll Posts for enhanced performance.
  • Bleed air provides thrust to roll post actuators for roll control.
Applications:
The F135 engine is specifically designed to power the F-35B STOVL aircraft, providing the necessary thrust for short takeoffs and vertical landings.
Additional Information:
For more details, visit the official websites: www.pw.utc.com and www.f135engine.com.
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Catalog excerpts

F135-1

Power for F-35B Short Takeoff and Vertical Landing (STOVL) Dependable Fifth-Generation Power from Land or Sea Product Fads Engine Characteristics Maximum thrust class Intermediate thrust class Short takeoff thrust class Hover thrust class Main engine Lift fan Roll post Length Main engine: Inlet diameter Max diameter Lift fan: Inlet diameter Max diameter ©2016 United Technologies Corporation. This document has been publicly released. This document does not contain any export regulated technical data. Features • Single-engine reliability and affordability derived from proven fifth-generation fighter technologies design, production and sustainment. • Advanced health monitoring and network logistics support designed to reduce sustainment costs increase mission readiness and enable weapon system availability. • World's most powerful fighter engine enables unequaled stealth combat capabilities and effectiveness. • LiftSystem is comprised of the Rolls-Royce LiftFan®, Driveshaft, 3 Bearing and Roll Posts. • Bleed air provides thrust-to-roll post actuators for roll control. Pratt & Whitney A United Technologies Company Visit us at: www.pw.utc.com www. f135engine. com

 Open the catalog to page 1
F135-2

F135 Power for F-35B Short Takeoff and Vertical Landing (STOVL) Photo Credit: Lockheed Martin JSF15-438 S16297-D.04.16 ©2016 United Technologies Corporation. This document has been publicly released. This document does not contain any export regulated technical data.

 Open the catalog to page 2

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