Users' questions

What is the airspeed of a C-130?

What is the airspeed of a C-130?

374 mph

Specifications
Primary Function Intratheater airlift.
Wingspan 132 feet, 7 inches (39.7 meters).
Speed 374 mph (Mach 0.57) at 20,000 feet (6,060 meters).
Ceiling 33,000 feet (10,000 meters) with 100,000 pounds (45,000 kilograms) payload.

What limits the rotational speed of a propeller?

One of the key factors limiting the speed of rotation being the interaction between the blades, optimize the speed of our propeller involve a search of the optimum number of blade. A further constraint imposed the rotational speed. This is the machine connected to the shaft..

How many hours can a C-130 fly without refueling?

The plane’s extreme range—it can travel 7,000 miles without refueling—means it often carries multiple crews and has provisions for up to 15 relief crew members.

What kind of propellers are on a C-130 Hercules?

Four Hamilton Standard electro-hydromatic, constant- speed, full feathering, reversible-pitch propellers are installed on the C-130 aircraft. Some of the configura- tions installed on the Hercules over the years include the 54H60-39,-63,-73, 75, 89, 91, 111, and 117.

What’s the maximum speed of a C-130 Hercules?

2,450 nm Maximum cruise speed …. 355 KTAS/660 km/hr *Higher payload allowable with wing relieving fuel **Higher zero fuel weight allowable with wing relieving fuel C-130J-30 Initial Cruise Altitude 28,000 ft C-130J-30 – 12.4 Minutes C-130H – 29 Minutes Time to Climb to Time to Climb to 18,000 ft (155k Lb.) 18,000 ft (164k Lb.)

How does the C-130 experience directional stability?

The C-130 experiences a marked reduction of directional stability at low dynamic pressures, high power settings, and at elevated side slip angles. This reduction in directional stability is manifested to the pilot as a low rudder force gradient (small rudder forces produce large side slip angles).

What are the specifications of a C-130J?

C-130J Specifications and Performance 1 External Dimensions 2 Weights and loadings. Payload, 2.5 g Max Zero-Fuel Weight, 2.5 g 3 Performance (at max normal takeoff weight, unless indicated otherwise)

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