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الصورة الرمزية عبدالرزاق احمد حاتم
عبدالرزاق احمد حاتم عبدالرزاق احمد حاتم غير متواجد حالياً
Flight Engineer66
 
تاريخ التسجيل: 06 - 06 - 2007
الدولة: سوريا
المشاركات: 837
شكر غيره: 0
تم شكره 6 مرة في 6 مشاركة
معدل تقييم المستوى: 392
عبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقدير

مشاهدة أوسمتي

عبدالرزاق احمد حاتم عبدالرزاق احمد حاتم غير متواجد حالياً
Flight Engineer66


الصورة الرمزية عبدالرزاق احمد حاتم

مشاهدة ملفه الشخصي
تاريخ التسجيل: 06 - 06 - 2007
الدولة: سوريا
المشاركات: 837
شكر غيره: 0
تم شكره 6 مرة في 6 مشاركة
معدل تقييم المستوى: 392
عبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقديرعبدالرزاق احمد حاتم يستحق الثقة والتقدير
افتراضي رد: تعرف ايش عن الـــC130

معلومات مفيده من الاخوة وشكرا على الموضوع
واليكم بعض المعلومات عنها:
C-130 Hercules
The C-130 Hercules primarily performs the intratheater portion of the airlift mission. The aircraft is capable of operating from rough, dirt strips and is the prime transport for paradropping troops and equipment into hostile areas. Basic and specialized versions perform a diversity of roles, including airlift support, DEW Line and Arctic ice resupply, aeromedical missions, aerial spray missions, fire-fighting duties for the US Forest Service, and natural disaster relief missions. In recent years, they have been used to bring humanitarian relief to many countries, including Haiti, Bosnia, Somalia, and Rwanda.
Four decades have elapsed since the Air Force issued its original design specification, yet the remarkable C-130 remains in production. The turbo-prop, high-wing, versatile "Herc" has accumulated over 20 million flight hours. It is the preferred transport aircraft for many US Government services and over 60 foreign countries. The basic airframe has been modified to hundreds of different configurations to meet an ever-changing environment and mission requirement. The C-130 Hercules has unsurpassed versatility, performance, and mission effectiveness. Early C-130A, B, and D versions are now retired.


Design Features

In its personnel carrier role, the C-130 can accommodate 92 combat troops or 64 fully equipped paratroops on side-facing seats. For medical evacuations, it carries 74 litter patients and two medical attendants. Paratroopers exit the aircraft through two doors on either side of the aircraft behind the landing-gear fairings. Another exit is off the rear ramp for airdrops.

The C-130 can deliver personnel, equipment or supplies either by landing or by various aerial delivery modes. Three primary methods of aerial delivery are used for equipment.
  • In the first, parachutes pull the load, weighing up to 42,000 pounds, from the aircraft. When the load is clear of the plane, cargo parachutes inflate and lower the load to the ground.
  • The second method, called the Container Delivery System, uses the force of gravity to pull from one to 16 bundles of supplies from the aircraft. When the bundles, weighing up to 2,200 pounds each, are out of the aircraft, parachutes inflate and lower them to the ground.
  • The Low Altitude Parachute Extraction System is the third aerial delivery method. With LAPES, up to 38,000 pounds of cargo is pulled from the aircraft by large, inflated cargo parachutes while the aircraft is five to 10 feet above the ground. The load then slides to a stop within a very short distance. Efforts are underway to increase the maximum load weights for LAPES aerial delivery to 42,000 pounds.
The C-130's design maximum gross weight is 155,000 pounds (175,000 pounds wartime) with a normal landing weight of 130,000 pounds. The operating weight is approximately 80,000 pounds. The airplane is capable of airlifting 92 ground troops, 64 fully equipped paratroopers, or 74 litter patients. It can also carry 45,000 pounds of cargo.
FUSELAGE: The fuselage is a semimonocoque design and divided into a flight station and a cargo compartment. Seating is provided for each flight station. The cargo compartment is approximately 41 feet long, 9 feet high, and 10 feet wide. Loading is from the rear of the fuselage. Both the flight station and the cargo compartment can be pressurized to maintain a cabin pressure-altitude of 5000 feet at an aircraft altitude of 28,000 feet.
WINGS: The full cantilever wing contains four integral main fuel tanks and two bladder-type auxiliary tanks. Two external tanks are mounted under the wings. This gives the C-l 30 a total usable fuel capacity of approximately 9680 U.S. gallons.
EMPENNAGE: A horizontal stabilizer, vertical stabilizer, elevator, rudder, trim tabs, and a tail cone make up the empennage. This section consists of an all-metal full cantilever semimonocoque structure. It is bolted to the aft fuselage section.
POWER PLANT: (prior to the C-130J) Four Allison turboprop engines are attached to the wings. The engine nacelles have cowl panels and access doors forward of a vertical firewall. Clam-shell doors are located aft of the vertical firewall. Air enters the engine through a scoop assembly at the front of the nacelle.
PROPELLERS: (prior to the C-130J) Four Hamiliton Standard electro-hydromatic, constant-speed, full feathering, reversible-pitch propellers are installed on each engine.
LANDING GEAR AND BRAKES: The modified tricycle-type landing gear consists of dual nose gear wheels and tandem mains. Main gear retraction is vertically, into fuselage fairings, and the nose gear folds forward into the fuselage. Power steering is incorporated into the nose gear. The landing gear design permits aircraft operation from rough, unimproved runways. The brakes are hydraulically operated, multiple-disc type. The braking system incorporates differential braking and parking brake control. A modulating anti-skid system is provided.
AUXILIARY POWER UNIT (APU) (C-130H): The APU supplies air during ground operation for engine starting and air conditioning. One 40 KVA AC generator is mounted on the APU as an additional AC power source. Emergency electrical power during flight is also available up to 20,000 feet.
GAS TURBINE COMPRESSOR (GTC) AND AIR TURBINE MOTOR (ATM) (C-130E): C-13OE model aircraft have a GTC which supplies bleed air for engine start, air conditioning, and operation of an ATM. The ATM powers a 20 KVA electrical generator to supply auxiliary electrical power on the ground only.
OIL: The C-130 has four independent oil systems with a 12 gallon capacity for each engine. Oil is serviced through a filler neck located on the upper right engine cowling.
FUEL: The fuel system consists of a modified manifold-flow type incorporating fuel crossfeed, single point refueling (SPR) and defueling, and fuel dumping. Latest USAF versions incorporate blue foam for fire suppression.
ELECTRICAL: AC electrical power for the C-130H model is provided by five 40 KVA generators, 4 driven by the engines and one driven by the APU. On the E model, the power is supplied by four 40 KVA engine-driven generators, and a 20 KVA generator driven by the ATM. DC power is provided from AC sources through four 200 ampere transfomer rectifiers and one 24 volt, 36 ampere-hour battery.
HYDRAULIC: Four engine-driven ***** supply 3000 psi pressure to the utility and booster systems. An electric AC motor-driven pump supplies pressure to the auxiliary system and is backed up by a handpump. The hydraulic system maintains constant pressure during zero or negative "g" maneuvers.
AIR CONDITIONING AND PRESSURIZATION: Two independent air conditioning systems for the flight deck and cargo compartment are operated from engine bleed air in flight and by the GTC/APU on the ground.
OXYGEN: Both models have a 25 liter liquid oxygen (LOX) type system which provides for 96 man-hours of oxygen at 25,000 feet. It uses diluter-demand automatic pressure-breathing regulators. Portable units are also provided. System pressure is maintained at 300 psi.
FLIGHT CONTROLS: The primary flight control system consists of conventional aileron, elevator, and rudder systems. Hydraulic power boost is incorporated in each system.
WING FLAPS: The wing flaps are high-lift, Lockheed-Fowler type and are of conventional design and construction. Normal operation is by hydraulic motor. Emergency operation is by manual crank.
ANTI-ICING: Engine bleed air is used for anti-icing the wing and empennage leading edges, the radome, (radome anti-icing may be removed in some models, check with aircraft forms) and engine inlet air ducts. Electrical heat provides anti-icing for the propellers, windshield, and pitot tubes.
AIRCRAFT DIMENSIONS:


Wing Span:

Length:
Height:
Horizontal Stabilizer:

132 feet 7 inches

97 feet 9 inches
38 feet 5 inches
52 feet 8 inches

Typical C-130 Cargo Dimensions:


Model


First Delivery


Last Delivery


C-130A


1956


Nov 1959


C-130B


1959


Mar 1963


C-130E


1962


Mar 1974


C-130H


1964


In Production


C-130H2


1978


1992


C-130H3


1992


1997


C-130J


1996


In Production


L-100


1964


Dec 1968


L-100-20


1968


Mar 1981


L-100-30


1970


In Production


C-130H-30


1980


1997


Specifications

Primary Function
Intratheater airlift.
Contractor
Lockheed Aeronautical Systems Company.
Power Plant
Four Allison T56-A-15 turboprops; 4,300 horsepower, each engine.
Length
97 feet, 9 inches (29.3 meters).
Height
38 feet, 3 inches (11.4 meters).
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.
Maximum Takeoff Weight
155,000 pounds (69,750 kilograms).
Operating Weight:
83,000 Pounds
Maximum Useable Fuel:
60,000 Pounds
Maximum Allowable Cabin Load:
36,000 Pounds
Normal Passenger Seats Available:
Up to 92 troops or 64 paratroops or 74 litter patients.
Maximum Number of Pallets:
5
Range
2,356 miles (2,049 nautical miles) with maximum payload;
2,500 miles (2,174 nautical miles) with 25,000 pounds (11,250 kilograms) cargo;
5,200 miles (4,522 nautical miles) with no cargo.
Unit Cost
$22.9 million (1992 dollars).
Crew
Five (two pilots, a navigator, flight engineer and loadmaster); up to 92 troops or 64 paratroops or 74 litter patients or five standard freight pallets.
Minimum Crew Complement
Four
(two pilots, one flight engineer, and one loadmaster)
Allows for a 16 hour crew duty day (12 hour for airdrop crews) (from show at the aircraft to parking at the final destination).
Crew Complement
[airdrop missions]
Six
crews will normally carry one navigator as well and an extra loadmaster in addition to the minimum crew complement.
Augmented Crew Complement
Nine
(three pilots, two navigators, two flight engineers, and two loadmasters)
Allows for a 18 hour crew duty day (from show at the aircraft to parking at the final destination)
Date Deployed
April 1955.
Inventory
Active force, 98; ANG, 20 Bs, 60 E's and 93 H's; Reserve, 606.


The most significant issue for the C-130 entails the reassignment of CONUS-based active duty C-130s from USACOM to USTRANSCOM. As the single manage for DoD transportation, the consolidation of these air mobility assets under USTRANSCOM lends further credence to USTRANSCOM’s single manager charter. Furthermore, as the Air Force component of USTRANSCOM, AMC now exercises both service authority (i.e., train, organize, equip, and provide) and operational control over these forces. This arrangement eliminates confusion and yields more effective and efficient service to the air mobility customer. (Theater CINCs will continue to exercise combatant command and operational control of overseas-assigned C-130 forces.)
التوقيع  عبدالرزاق احمد حاتم
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