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F-35 Air Vehicle Technology Overview

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F-35 Air Vehicle Technology Overview ( f-35-air-vehicle-technology-overview )

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resultant systems incorporated into the F-35 have been proven to provide excellent technical performance and reliability. They also provide a backbone for future systems growth through the expected long life of the F-35 program. The F-35 propulsion systems incorporating the numerous technology upgrades have driven an unprecedented capability in performance. This has enabled the aircraft’s unique performance capabilities, particularly in the F-35B STOVL variant. The final F-35 configuration incorporated a DSI, LO axisymmetric engine thrust nozzle, and unique STOVL propulsion system integrating the LiftFan and three-bearing swivel nozzle. These systems enabled the development of the F-35 variants, each providing exceptional performance and serving as the basis for long-term growth and capability improvements. Acknowledgments The author thanks Jeff Hamstra, Rick Mange, and JD McFarlan for their leadership in pursuing the entire family of related papers. The author gives special thanks also to graphic artists Daniel Buck and Mark Lawhon, and to Joey Sikorski for help in pulling together a lot of details that went into this report. References [1] Barhydt, J., Carter, H., and Weber, D., "Subsystem Integration Technology (SUIT) Phase I," WL-TR-93-3031, July 1993. [2] Blanding, D., Schlundt, D., and Aldana, J., "Subsystem Integration Technology (SUIT)," WL-TR-92-3105, December 1992. [3] Hill, B., Stem, P., Ho, Y., and Martin, D., "Subsystem Integration Technology (SUIT),” Executive Summary, Vol. 1, WL-TR- 92-3115, October 1992. [4] Hill, B., Stem, P., Ho, Y., and Martin, D., "Subsystem Integration Technology (SUIT),” Phase I Report, Vol. 2, WL-TR-92- 3116, October 1992. [5] Hill, B., Stem, P., Ho, Y., and Martin, D., "Subsystem Integration Technology (SUIT),” Phase II Report, Vol. 3, WL-TR-92- 3117, October 1992. [6] Hill, B., Stem, P., Ho, Y., and Martin, D., "Subsystem Integration Technology (SUIT),” Phase III Report, Vol. 4, WL-TR-92- 3118, October 1992. [7] Carter, H., Rupe, K., Mattes, R., and Wiese, D., "Subsystem Integration Technology (SUIT),” Phase II Report, WL-TR-96- 3065, May 1997. [8] Terrier, D., Hodge, E., Eicke, D., and Roberts, J., "Vehicle Integration Technology Planning Study (VTIPS)," WL-TR-96- 2077, April 1996. [9] Weber, D., Hill, B., and Van Hom, S., "Vehicle Integration Technology Planning Study (VTIPS)," WL-TR-97-3036, February 1997. [10] Eicke, D., "Joint Strike Fighter Integrated Subsystems Technology (J/IST) Power and Actuation Flight Demonstration Program," AFRL-PR-WP-2001-2036, January 2001. [11] Carter, H., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Executive Summary, Vol. 1, AFRL-VA-WP-TR-2001-3028, June 2001. [12] Rupe, K. and Carter, H., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 2, Program Integration, AFRL-VA-WP-TR-2001-3029, June 2001. [13] Heydrich, H. and Roddiger, H., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 3, Thermal/Energy Management Module (T/EMM) Turbomachine, AFRL-VAWP-TR-2001-3030, June 2001. [14] Dastur, N. and Roddiger, H., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 4, Thermal/Energy Management Module (T/EMM) System Integration, AFRL-VA- WP-TR-2001-3031, June 2001. [15] Anderson, G. and Waffner, W., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 5, High Power Electric Actuation, AFRL-VA-WPTR-2001-3032, June 2001. [16] Torchia, D. and Rupe, K., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 6, Power Management Integration, AFRL-VA-WP-TR-2001-3033, June 2001. [17] Anderson, J. and Roddiger, H., "Joint Strike Fighter (JSF)/Integrated Subsystems Technology (J/IST) Demonstration Program,” Vol. 7, Engine Integration, AFRL-VAWP-TR-2001-3034, June 2001. [18] Eicke, D., "Joint Strike Fighter Integrated Subsystems Technology (J/IST) Power and Actuation Flight Demonstration Program,” Executive Summary, AFRL-PR-WP-2001-2077, January 2001. [19] Iya, S., Harlan, R., and Hawkins, L., "LCC and War Fighting Assessment of J/IST Suite," AFRL-VA-WP-TR-2000-3016, March 1999. [20] Hamstra, J. W., McCallum, B. N., McFarlan, J. D., and Morehouse, J. A., “Development, Verification and Transition of an Advanced Engine Inlet Concept for Combat Aircraft Application,” NATO RTO Paper MP-121-P-43, October 2003. [21] Hehs, E., “Diverterless Supersonic Inlet,” Code One, July 2000. [22] Scharnhorst, R. S., “An Overview of Military Aircraft Supersonic Inlet Aerodynamics,” AIAA Paper 2012-0013, January 2012. [23] Sobester, A., “Tradeoffs in Jet Inlet Design: A Historical Perspective,” Journal of Aircraft, Vol. 44, No. 3, May 2007. Approved for public release 5/8/18, JSF18-365 27

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