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David
Wed December 11, 2002 4:33pm
"Two Coast Guard-manned L

"Two Coast Guard-manned LST's open their great jaws in the surf that washes on Leyte Island beach, as soldiers strip down and build sandbag piers out to the ramps to speed up unloading operations." 1944.
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David
Wed December 11, 2002 4:33pm
"Marines unloading Japane

"Marines unloading Japanese POW from a submarine returned from war patrol." Lt. Comdr. Horace Bristol, ca. May 1945.
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David
Fri December 13, 2002 12:40pm
Unloading American caisso

Unloading American caissons and limbers for 75mm guns
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David
Thu January 16, 2003 10:39am
HH/MH-60G Pave Hawk


Function: Twin-engine, medium lift, Combat Search and Rescue and Special Operations Support helicopter.








Description: The HH/MH-60G Pave Hawk is a twin-engine helicopter used by the Airforce in a CSAR/SOS role. Based on the basic S-60 Blackhawk utility helicopter airframe, the Pave Hawk has been optimized for low level insertions and extractions, self defense, enemy small arms fire suppression, and bulk cargo and troop transport. To extend their range, Pave Hawks are equipped with a retractable in-flight refueling probe and internal auxiliary fuel tanks. The HH/MH-60G variant is also equipped with an externally mounted 600 pound capacity hoist and sliding doors on each side of the troop and cargo compartment to allow rapid loading and unloading. The HH/MH-60G is capable of transporting a 8,000 pound load externally and can be equipped with the external stores support system.





General Characteristics, HH/MH-60G Pave Hawk



Contractors:
United Technologies/Sikorsky Aircraft Company





Power Plant:
Two General Electric T700-GE-700 or T700-GE-701C engines producing 1,560-1,630 shaft horsepower





Length:
64 feet, 8 inches (17.1 meters)





Height:
16 feet, 8 inches (4.4 meters)





Rotor Diameter:
53 feet 8 inches (16.4 meters)





Maximum Take-off Weight:
22,000 pounds (9,900 kilograms)





Speed:
180 knots maximum





Range:
504 nautical miles (unlimited with air refueling)





Crew:
Two pilots, one flight engineer, one gunner and up to 10 troops









Navigation Sensors:
VHF/UHF DF


TACAN


TACNAV


Doppler Radar


Radar Altimeter


GPS (Provisions)


Forward Looking Infra Red (FLIR) system





Armament:
Variable, but may include any combination of the following:


Two GCAL-50 machine guns


Two GAU-17A 7.62mm miniguns


2.75" Hydra 70 Folding Fin Aerial Rocket pods


FIM-92A Stinger Surface to Air Missiles


AGM-65 Maverick Air to Ground Missiles


AGM-114 Hellfire Air to Ground Missiles





Countermeasures:
Infrared (IR) Jamming System


Chaff and Flare Dispensers (2)


Radar Warning Receiver


Hover IR Suppressor System
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David
Thu January 16, 2003 11:05pm
M1084 Standard Cargo Truc


Function: Transport.






Description: The M1084 Standard Cargo Truck with MHE is designed to transport cargo and soldiers. The M1084 has a payload capacity of 10,000 pounds and lift capacity of 2,500 to 5,000 pounds using the on board MHE. The cargo bed side rails are hinged for the ease of loading and unloading cargo. The cargo bed can be equipped with an optional bench seat kit for transport of soldiers. The bench seats are constructed of a non-wood material and attach to the cargo bed side rails. The seats can be folded down and stowed when not in use. Soldiers are assisted climbing in and out of the cargo bed area with the aid of a ladder stowed on the vehicle when not in use. A canvas and bows kit is provided to keep soldiers and cargo protected from the elements. The M1084 can be equipped with a self-recovery winch capable of fore/aft vehicle recovery operations. The winch has 280 feet of line capacity and 15,500 pounds bare drum line pull at 110% overload.
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David
Sat January 18, 2003 8:34am
The MH-60G's primary wart

The MH-60G's primary wartime missions are infiltration, exfiltration and resupply of special operations forces in day, night or marginal weather conditions. Other missions include combat search and rescue. The MH-60G is equipped with an all-weather radar which enables the crew to avoid inclement weather. To extend their range, Pave Hawks are equipped with a retractable in-flight refueling probe and internal auxiliary fuel tanks. Pave Hawks are equipped with a rescue hoist with a 200-foot (60.7 meters) cable and 600-pound (270 kilograms) lift capacity. All MH-60G's have an automatic flight control system to stabilize the aircraft in typical flight altitudes. They also have instrumentation and engine and rotor blade anti-ice systems for all-weather operation. The non-retractable landing gear consists of two main landing gears and a tail wheel. Aft sliding doors on each side of the troop and cargo compartment allow rapid loading and unloading. External loads can be carried on an 8,000-pound (3,600 kilograms) capacity cargo hook. Pave Hawks are equipped with folding rotor blades and a tail stabilator for shipboard operations and to ease air transportability.
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David
Sat January 18, 2003 9:42am
Rating: 8 
The C-9 is a twin-engine,

The C-9 is a twin-engine, T-tailed, medium-range, swept-wing jet aircraft used primarily for Air Mobility Command's aeromedical evacuation mission. The Nightingale is a modified version of the McDonnell Douglas Aircraft Corporation's DC-9. It is the only aircraft in the inventory specifically designed for the movement of litter and ambulatory patients. The C-9A's airlift capability to carry 40 litter patients, 40 ambulatory and four litter patients, or various combinations thereof, provides the flexibility for Air Mobility Command's worldwide aeromedical evacuation role. A hydraulically operated folding ramp allows efficient loading and unloading of litter patients and special medical equipment.
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David
Sat January 3, 2004 9:38pm
An-124 Condor

Function: High payload, long range cargo aircraft.



History: Introduced in 1982 as a long range, heavy lift cargo and troop transport aircraft, the Antonov An-124 Ruslan (NATO designation Condor) is currently the world's largest and heaviest payload aircraft in production in the world. Outclassing the C-5 Galaxy by nearly 20 tons in payload capacity, and the Ilyushin Il-76 by more than 100 tons, the An-124 is only exceeded in lifting ability by the special purpose An-225 Mriya (NATO designation Cossack) which was purpose built to transport the Russian space shuttle, and of which only two were built.


Currently in production at the AVIASTAR facility in Ulyanovsk and the AVIANT State Aviation Plant in Kiev, the An-124, in addition to serving with the Russian military as a long range high payload cargo aircraft capable of delivering or airdropping troops, and equipment, is also in service with a number of civilian organizations as a dedicated cargo transport. Antonov Airlines, Volga-Dniepr, and Poliot all employ the An-124, using it to transport heavy and over sized equipment such as hydraulic turbines, mobile cranes, railway locomotives, earthmovers and dump trucks, and sailing vessels. The An-124 is even capable of transporting other aircraft, ferrying partially disassembled passenger planes to customers worldwide.


To facilitate the loading and unloading of cargo, the nose section is hinged to open upwards, and the tail section is fitted with a pair of clamshell doors. Both nose and tail sections are equipped with integral loading ramps. In addition, the An-124 also employs two traveling cranes, two winches, a rollgang and tie down equipment which limit it's dependence on ground equipment for cargo handling and manipulation. The Ruslan is equipped with multi leg, self-orienting landing gear and is rough surface capable. The landing gear height can be adjusted on the ground, to facilitate loading cargo.


In addition to the An-124-100 currently in production, Air Foyle (UK) in conjunction with Antonov and Aviastar has proposed the construction of two new versions, the An-124-210, and the An-124-100M. Both versions will be equipped with Western and Russian digital instruments and displays which will reduce the crew size from 6 to 4. In addition, both will be equipped with a traffic alert collision and avoidance system, ground proximity warning system and a satellite communications system. The 210 will be outfitted with Rolls-Royce RB211-52H-T engines, while the 100M will be equipped with the Series 3 D-18 engines, produced by the Progress Design Bureau in Zaporozhe. Each of these engine upgrades will increase the Ruslan's range by 10% and reduce take off distance.



Description: Typical of most cargo aircraft, the An-124 body forms a thick oval cross-section, with a tapered aft section and rounded nose to facilitate cargo handling. The fuselage is of a twin deck design, the upper deck being the flight deck, and the lower deck serving as the cargo hold. On the flight deck are the cockpit, with stations for the six crewmembers, a relief crew compartment, and seating for an additional 88 passengers. The loadmaster's station is on the cargo deck.


The wings are mounted high on the fuselage at a negative dihedral, are tapered and swept, with a relatively high cross-section to increase efficiency and range. The four Lotarev D-18T turbofans are mounted on pylons underneath the wings. The horizontal stabilizers are also swept back and tapered, and are mounted at mid level on the fuselage, aft of the vertical stabilizer.



General Characteristics, AN-124 Condor


Power Plant:
Four D-18T turbofans (An-124-100)


Four D-18T Series 3 (An-124-100M)


Four RB211-524H-T (An-124-210)



Thrust:
229 kN (153,558 pounds)


An-124-210: 264 kN (177,027 pounds)



Length:
69.1 meters (226.4 feet)



Height:
21.08 meters (69.2 feet)



Wingspan:
73.3 meters (240.5 feet)



Cargo Hold Dimensions:
Floor length including ramps: 36.5 meters


Width at floor level: 6.4 meters


Height: 4.4 meters


Volume cargo hold: 1,270 cubic meters



Speed:
800 to 850 kmh


Cruise speed at an altitude of 9 km: 750 to 800 kmh




Ceiling:
12,000 meters (39,370 feet)



Load-Carrying Capacity:
120 tons using a 2,800 meter runway (2300 meters for An-124-210)


150 tons using a 3,000 meter runway (2500 meters for An-124-210)



Maximum Takeoff Weight:
392 tons



Range:
With maximum fuel: 13,300 kilometers (7,980 miles) (15,250 for An-124-210)


With 40-ton payload: 10,960 kilometers (6,576 miles) (12,730 for An-124-210)


With 120-ton payload: 5,030 kilometers (3,018 miles) (5,950 for An-124-210)



Crew:
Seven (An 124)
Four (An-124-100)
Four (An-124-100M)
Three (An-124-210)



Runway:


3000 meters (2,420 for An-124-210)


Takeoff run on concrete runway: 2520 meters (2,420 for An-124-210)


Landing roll on concrete runway: 900 meters




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David
Sat January 3, 2004 10:35pm
T-AK - LASH Type Cargo Sh

Function: The lighterage aboard ships are assigned to Military Sealift Command's Prepositioning Program. SS Green Valley, SS Green Harbour, SS Austral Rainbow and MV Jeb Stuart are all stationed out of Diego Garcia in the Indian Ocean.



History: The Green Valley was chartered by MSC in 1992. Central Gulf Lines owns and operates the Green Valley. The Austral Rainbow and Green Harbour are also owned and operated by Central Gulf Lines. The Austral Rainbow was first acquired by MSC in 1987 and has had severed successive charters with MSC. The Green Harbour was acquired in 1985. The Jeb Stuart is owned and operated by Waterman Steamship Company under contract to MSC. The Jeb Stuart was chartered in 1992.



Description: The LASH ships are capable of carrying both barges and containers. All four ships are self-sustaining, meaning they are capable of unloading themselves in areas without developed harbor infrastructure.



General Characteristics, Green Valley Class


Builders:
Avondale Shipyards



Power Plant:
Three Babcock & Wilcox boilers, 580 psi (40.8 kg/cm2); 8250F (4400C); one De Laval turbine (Westinghouse in TAFS 6); 22,000 hp (16.4MW) sustained; one shaft



Length, Overall:
820 feet (249.94 meters)



Beam:
100 feet (30.48 meters)




Displacement:
46,152 long tons (46,892.65 metric tons) full load



Speed:
16 knots (18.41 mph, 29.63 kph)



Crew:
24 civilians





General Characteristics, Austral Rainbow Class


Builders:
Avondale Shipyards



Power Plant:
Two combustion engineering boilers; 1,100 psi; two De Val turbines; 32,000 hp; one shaft



Length, Overall:
820 feet (249.94 meters)



Beam:
100 feet (30.48 meters)




Displacement:
39,277 long tons (39,907.32 metric tons) full load



Speed:
16 knots (18.41 mph, 29.63 kph)



Crew:
24 civilians





General Characteristics, Jeb Stuart Class


Builders:
Sumitomo Shipbuilding



Power Plant:
One Sulzer 9RND90 diesel; 26,000 horsepower



Length, Overall:
857 feet (261.21 meters)



Beam:
106 feet (32.31 meters)




Displacement:
66,629 long tons (67,698.27 metric tons) full load



Speed:
16 knots (18.41 mph, 29.63 kph)



Cargo Capacity:
1,191,683 cubic feet



Crew:
24 civilians




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