> For the complete documentation index, see [llms.txt](https://docs.miltechsimulations.com/llms.txt). Markdown versions of documentation pages are available by appending `.md` to page URLs; this page is available as [Markdown](https://docs.miltechsimulations.com/miltech-simulations-microsoft-c-17-globemaster-iii/the-aircraft/performance-characteristics.md). # Performance Characteristics {% hint style="info" %} Please note that the publicly known performance figures for the C17 Globemaster are limited due to the fact that the aircraft is in active military service. Specific performance figures are unavailable. {% endhint %} | Wingspan to Winglet Tip | 169.8 ft (51.74 m) | | ------------------------------- | ------------------------------------------------------------- | | Length | 174 ft (53.04 m) | | Height at Tail | 55.1 ft (16.79 m) | | Fuselage Diameter | 22.5 ft (6.86 m) | | Number of Engines | Four (4) | | Engine Type | F117-PW-100 | | Thrust per Engine | 40,440 lbs Each | | Area | 3,800 sq. ft. (353 sq. m) | | Aspect Ratio | 7.165 | | Sweep Angle | 25 degrees | | Airfoil Type | Supercritical | | Flaps | Fixed-vane, double-slotted, simple-hinged | | Area | 845 sq. ft. (78.50 sq. m) | | Span | 65 feet (19.81 m) | | Aspect Ratio | 5.0 | | Sweep | 27 degrees | | Maximum Zero Fuel Weight (MZFW) | 282,500 lb (128,140 kg) | | Max Takeoff Weight (MTOW) | 585,000 lb (265,352 kg) | | Max Landing Weight, Full Flaps | 502,100 lb (227,748 kg) | | Fuel Capacity | 35,546 US gal | | Capacity | 170,900 lb (77,519 kg) | | Capacity, in Pallets | 18 463L Master Pallets | | Capacity, in Troops | 134 Troops, seated | | Capacity, in Paratroopers | 102 Paratroopers, seated | | Capacity, in Vehicles | One heavy tank, or Three Armored Vehicles, or 10 HWMVVs | | Capacity, in Aircraft | One CH47 Helicopter Fuselage, or two H60 Helicopter Fuselages | | Cruise Speed | 450 kn (Mach 0.74-0.79) | | Range | 2,420 nmi with 157,000 lb payload | | Ferry Range | 6,230 nmi | | Service Ceiling | 45,000 ft | | Takeoff Run at MTOW | 8,200 ft | | Takeoff Run at 395,000 lbs | 3,000 ft | | Landing Distance | 3,500 ft | --- # Agent Instructions This documentation is published with GitBook. GitBook is the documentation platform designed so that both humans and AI agents can read, navigate, and reason over technical content effectively. Learn more at gitbook.com. ## Querying This Documentation If you need additional information that is not directly available in this page, you can query the documentation dynamically by asking a question. Perform an HTTP GET request on the current page URL with the `ask` query parameter, and the optional `goal` query parameter: ``` GET https://docs.miltechsimulations.com/miltech-simulations-microsoft-c-17-globemaster-iii/the-aircraft/performance-characteristics.md?ask=&goal= ``` `ask` is the immediate question: it should be specific, self-contained, and written in natural language. `goal` is optional and describes the broader end goal you are ultimately trying to accomplish on behalf of the user. GitBook uses it to tailor the answer towards what is most useful for that goal. The response will contain a direct answer to the question and relevant excerpts and sources from the documentation. Use this mechanism when the answer is not explicitly present in the current page, you need clarification or additional context, or you want to retrieve related documentation sections.