Homieville
05-03-2006, 23:32
Welcome to the Advanced Flight Storefront. -=You will have over 20 different Aircrafts to choose from in Mid March=-
Additional Store Links
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www.forums.jolt.co.uk/showthread.php?p=10531427#post10531427
Rules~
- No spaming in this storefront
- Topics should be related to Helicopters, and military devices
- Nations with a low rated economy are not aloud to buy these aircrafts.
-Do your own math
Discounts~
- Discounts are 15% from the purchase price
-Discounts will be rewarded to loyal costumers that have purchased something from this storefront at least 5 times.
-Nation Discounts
-Flame From Hell
-Ardchoille
-Polska55
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First Class Attackers
http://www.globalsecurity.org/military/systems/aircraft/images/dvd-226-5.jpg
Type----Bird of Prey
Primary Function
Contractor Boeing
Power Plant One Pratt & Whitney JT15D-5C turbofan engine
Length 47 feet
Weight 7,400 pounds (23,625 kilograms)
Wingspan 23 feet
Speed 260 kts
Unit Cost $30,000,000
Crew One
Production Year 2003
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First Class Helicopter
http://www.bellhelicopter.com/images/CV22_main_750x250_46558.jpg
Type----The V-22
About---- This helicopter is a unique one that only 20 have been manufactered in Japan.
U.S. Marine Corps
Principle combat aircraft to enable Expeditionary Maneuver Warfare (EMW) and Ship To Objective Maneuver (STOM)
---Airspeed 240 kts Cruise speed (MV-22)
230 kts Cruise speed (CV-22)
275 KTAS Cruise speed (3000'/91.5 deg F)
305 KTAS Max speed (15,000' /45 deg F
--- has two missiles that are directly nevigated to the enemy.
-- Can fit over 4 soldiers. This helicopter is mainly used for transportation and upcoming in air missile launches
-Price $108,000,000
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First Class Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/sh-3-DN-SC-96-00128.jpg
Type----The H3 Sea King
Specs
-Main rotor diameter 62 ft.
-Fuselage Length 73 ft. 0 in.
-Height 18 ft. 1 in.
-Weight 22,050 lbs. loaded
-Armament Provisions for two .50-cal. machine guns
-Engines Two General Electric T58-GE-5 turboshaft engines of 1,500 hp. each
-Crew Three
-Cost $796,000
-Maximum speed 177 mph.
-Cruising speed 154 mph.
-Range 779 miles with external fuel tanks
-Service Ceiling 21,000 ft.
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Second Class Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/hh-65-iaf6.jpg
Type----HH-65A Dolphin
Specs
Mission Short range recovery (SRR) helicopter twin-engine
Replaced aging HH-52A fleet
Manufacturer Aerospatiale
Overall Length 38 ft.
Rotor Diameter 39 ft.
Overall Height 13 ft.
Maximum Gross Weight 9,200 lbs
Empty Mission Weight 6,092 lbs
Fuel Capacity 291 gallons / 1,900 pounds
Powerplants Two Lycoming LTS-101-750B-2 engines rated at 742 Shaft HP each
Maximum Range 300 nautical miles
Radius of Action 150 nautical miles
Maximum Speed 165 knots
Cruising Speed 120 knots
Max Endurance 3.5 hours
Service Ceiling (Hover) 7,510 feet above sea level
Cargo Sling Capacity 2000 lbs
Rescue Hoist Capacity 600 lbs
Crew Number of Pilots: 2
Number Flight Crew: 2
Inventory 80 - Operational Aircraft
14 - Storage or Support Aircraft
94 - Total Number of Aircraft
cost $600,000
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Lux Generals Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/s-92-04-s.jpg
Type---- S-92 Helibus
Specs
Fuselage length 17.32 m
Length overall, rotor turning 20.85 m
Height 6.45 m overall
Width 3.89 m over sponsons
Main rotor diameter 17.71 m
Main rotor disk 231.55 sq m
Tail rotor diameter 3.35 m
Tail rotor disk area 8.83 sq m
Gross weight, internal load 25,500 lb
Empty weight, civil transport 15,500 lb
Empty weight, international utility 15,200 lb
Gross weight, external load 26,800 lb
External cargo hook capacity 10,000 lb
Propulsion Two CT7-8 Engines
Maximum cruise speed 151 kt
Best range speed 136 kt
Range 475 nm
Hover OGE 5,500 ft
Hover IGE 10,175 ft
cost $7,000,000
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First Class ASW's
http://www.globalsecurity.org/military/systems/aircraft/images/s-3b-hookdown.jpg
Type----S-3B-Viking
Specs
Primary Function Antisubmarine Warfare and Sea Surveillance
Contractor Lockheed-California Company
Propulsion Two General Electric TF-34-GE-400B turbofan engines (9,275 pounds of thrust each)
Length 53 feet 4 inches (16 meters)
Wingspan 68 feet 8 inches (20.6 meters)
Height 22 feet 9 inches (6.9 meters)
Weight Max design gross take-off: 52,539 pounds (23,643 kg)
Speed 450 knots (518 mph, 828.8 kph)
Ceiling 40,000 feet
Range 2,300+ nautical miles (2,645 statute miles, 4232 km)
Armament Up to 3,958 pounds (1,781 kg)
AGM-84 Harpoon
AGM-65 Maverick missiles
torpedoes, mines, rockets and bombs.
Crew Four
IOC 1975
Unit Cost $27 million
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First Class Transporters and Attackers
http://www.globalsecurity.org/military/systems/aircraft/images/c-5b-19990422-f-0024f-004.jpg
Type----C-5
Specs
Primary Function strategic airlift.
Contractor Lockheed-Georgia Co.
Length 247 feet, 10 inches (75.3 meters).
Height At Tail 65 feet, 1 inch (19.8 meters).
Wingspan 222 feet, 9 inches (67.9 meters).
Stabilizer Span 68 feet, 9 inches (20.8 meters).
Cargo Compartment Height 13 feet, 6 inches (4.10 meters); width 19 feet (5.76 meters).
Maximum Takeoff Weight 769,000 pounds (346,500 kilograms).
Maximum Wartime Takeoff Weight 840,000 pounds (378,000 kilograms).
Operating Weight 374,000 lb
Max Payload, 2.5g 216,000 lb
Max Payload, 2.25g 261,000 lb
Load 291,000 pounds (130,950 kilograms) maximum wartime payload.
Power Plant Four General Electric TF39-GE-1C turbofan engines.
Thrust 41,000 pounds (18,450 kilograms), each engine.
Takeoff/Landing Distances 12,200 feet (3,697 meters) takeoff fully loaded;
4,900 feet (1485 meters) land fully loaded.
Total Fuel Capacity 51,154 US gal
Max Payload Range 2,960 NM
Range 5,940 miles (5,165 nautical miles) empty.
Ferry Range 6,985 NM
Speed 541 mph (Mach 0.72)
Design Cruise Speed 489 kt
Long Range Cruise Speed 465 kt
Max Rate of Climb (MGW) 1,610 fpm
Max Operating Altitude 43,500 ft
Ceiling 34,000 feet (10,303 meters) with a 605,000-pound (272,250-kilogram) load.
Accommodations Upper deck seats 73 passengers; forward upper deck seats six, a relief crew of seven, and eight mail or message couriers. The flight deck has work stations for the entire crew. The upper deck's forward and rear compartments have galleys for food preparation and lavatories.
Sensors An automatic trouble-shooting system constantly monitors more than 800 test points in the various subsystems of the C-5. The Malfunction Detection Analysis and Recording System uses a digital computer to identify malfunctions in replaceable units. Failure and trend information is recorded on magnetic tape for analysis by maintenance people.
Crew Six (pilot, co-pilot, two flight engineers, two loadmasters)
Date Deployed December 1969 (for training); June 1970 (operational); December 1984 (to Reserve).
Inventory Active-force, 70; ANG, 11; Reserve, 28.
Cost C-5A, $163.4 million; C-5B, $167.7 million
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Additional Store Links
{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{}{
www.forums.jolt.co.uk/showthread.php?p=10531427#post10531427
Rules~
- No spaming in this storefront
- Topics should be related to Helicopters, and military devices
- Nations with a low rated economy are not aloud to buy these aircrafts.
-Do your own math
Discounts~
- Discounts are 15% from the purchase price
-Discounts will be rewarded to loyal costumers that have purchased something from this storefront at least 5 times.
-Nation Discounts
-Flame From Hell
-Ardchoille
-Polska55
**********************************************************
First Class Attackers
http://www.globalsecurity.org/military/systems/aircraft/images/dvd-226-5.jpg
Type----Bird of Prey
Primary Function
Contractor Boeing
Power Plant One Pratt & Whitney JT15D-5C turbofan engine
Length 47 feet
Weight 7,400 pounds (23,625 kilograms)
Wingspan 23 feet
Speed 260 kts
Unit Cost $30,000,000
Crew One
Production Year 2003
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First Class Helicopter
http://www.bellhelicopter.com/images/CV22_main_750x250_46558.jpg
Type----The V-22
About---- This helicopter is a unique one that only 20 have been manufactered in Japan.
U.S. Marine Corps
Principle combat aircraft to enable Expeditionary Maneuver Warfare (EMW) and Ship To Objective Maneuver (STOM)
---Airspeed 240 kts Cruise speed (MV-22)
230 kts Cruise speed (CV-22)
275 KTAS Cruise speed (3000'/91.5 deg F)
305 KTAS Max speed (15,000' /45 deg F
--- has two missiles that are directly nevigated to the enemy.
-- Can fit over 4 soldiers. This helicopter is mainly used for transportation and upcoming in air missile launches
-Price $108,000,000
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First Class Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/sh-3-DN-SC-96-00128.jpg
Type----The H3 Sea King
Specs
-Main rotor diameter 62 ft.
-Fuselage Length 73 ft. 0 in.
-Height 18 ft. 1 in.
-Weight 22,050 lbs. loaded
-Armament Provisions for two .50-cal. machine guns
-Engines Two General Electric T58-GE-5 turboshaft engines of 1,500 hp. each
-Crew Three
-Cost $796,000
-Maximum speed 177 mph.
-Cruising speed 154 mph.
-Range 779 miles with external fuel tanks
-Service Ceiling 21,000 ft.
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Second Class Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/hh-65-iaf6.jpg
Type----HH-65A Dolphin
Specs
Mission Short range recovery (SRR) helicopter twin-engine
Replaced aging HH-52A fleet
Manufacturer Aerospatiale
Overall Length 38 ft.
Rotor Diameter 39 ft.
Overall Height 13 ft.
Maximum Gross Weight 9,200 lbs
Empty Mission Weight 6,092 lbs
Fuel Capacity 291 gallons / 1,900 pounds
Powerplants Two Lycoming LTS-101-750B-2 engines rated at 742 Shaft HP each
Maximum Range 300 nautical miles
Radius of Action 150 nautical miles
Maximum Speed 165 knots
Cruising Speed 120 knots
Max Endurance 3.5 hours
Service Ceiling (Hover) 7,510 feet above sea level
Cargo Sling Capacity 2000 lbs
Rescue Hoist Capacity 600 lbs
Crew Number of Pilots: 2
Number Flight Crew: 2
Inventory 80 - Operational Aircraft
14 - Storage or Support Aircraft
94 - Total Number of Aircraft
cost $600,000
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Lux Generals Helicopter
http://www.globalsecurity.org/military/systems/aircraft/images/s-92-04-s.jpg
Type---- S-92 Helibus
Specs
Fuselage length 17.32 m
Length overall, rotor turning 20.85 m
Height 6.45 m overall
Width 3.89 m over sponsons
Main rotor diameter 17.71 m
Main rotor disk 231.55 sq m
Tail rotor diameter 3.35 m
Tail rotor disk area 8.83 sq m
Gross weight, internal load 25,500 lb
Empty weight, civil transport 15,500 lb
Empty weight, international utility 15,200 lb
Gross weight, external load 26,800 lb
External cargo hook capacity 10,000 lb
Propulsion Two CT7-8 Engines
Maximum cruise speed 151 kt
Best range speed 136 kt
Range 475 nm
Hover OGE 5,500 ft
Hover IGE 10,175 ft
cost $7,000,000
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First Class ASW's
http://www.globalsecurity.org/military/systems/aircraft/images/s-3b-hookdown.jpg
Type----S-3B-Viking
Specs
Primary Function Antisubmarine Warfare and Sea Surveillance
Contractor Lockheed-California Company
Propulsion Two General Electric TF-34-GE-400B turbofan engines (9,275 pounds of thrust each)
Length 53 feet 4 inches (16 meters)
Wingspan 68 feet 8 inches (20.6 meters)
Height 22 feet 9 inches (6.9 meters)
Weight Max design gross take-off: 52,539 pounds (23,643 kg)
Speed 450 knots (518 mph, 828.8 kph)
Ceiling 40,000 feet
Range 2,300+ nautical miles (2,645 statute miles, 4232 km)
Armament Up to 3,958 pounds (1,781 kg)
AGM-84 Harpoon
AGM-65 Maverick missiles
torpedoes, mines, rockets and bombs.
Crew Four
IOC 1975
Unit Cost $27 million
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First Class Transporters and Attackers
http://www.globalsecurity.org/military/systems/aircraft/images/c-5b-19990422-f-0024f-004.jpg
Type----C-5
Specs
Primary Function strategic airlift.
Contractor Lockheed-Georgia Co.
Length 247 feet, 10 inches (75.3 meters).
Height At Tail 65 feet, 1 inch (19.8 meters).
Wingspan 222 feet, 9 inches (67.9 meters).
Stabilizer Span 68 feet, 9 inches (20.8 meters).
Cargo Compartment Height 13 feet, 6 inches (4.10 meters); width 19 feet (5.76 meters).
Maximum Takeoff Weight 769,000 pounds (346,500 kilograms).
Maximum Wartime Takeoff Weight 840,000 pounds (378,000 kilograms).
Operating Weight 374,000 lb
Max Payload, 2.5g 216,000 lb
Max Payload, 2.25g 261,000 lb
Load 291,000 pounds (130,950 kilograms) maximum wartime payload.
Power Plant Four General Electric TF39-GE-1C turbofan engines.
Thrust 41,000 pounds (18,450 kilograms), each engine.
Takeoff/Landing Distances 12,200 feet (3,697 meters) takeoff fully loaded;
4,900 feet (1485 meters) land fully loaded.
Total Fuel Capacity 51,154 US gal
Max Payload Range 2,960 NM
Range 5,940 miles (5,165 nautical miles) empty.
Ferry Range 6,985 NM
Speed 541 mph (Mach 0.72)
Design Cruise Speed 489 kt
Long Range Cruise Speed 465 kt
Max Rate of Climb (MGW) 1,610 fpm
Max Operating Altitude 43,500 ft
Ceiling 34,000 feet (10,303 meters) with a 605,000-pound (272,250-kilogram) load.
Accommodations Upper deck seats 73 passengers; forward upper deck seats six, a relief crew of seven, and eight mail or message couriers. The flight deck has work stations for the entire crew. The upper deck's forward and rear compartments have galleys for food preparation and lavatories.
Sensors An automatic trouble-shooting system constantly monitors more than 800 test points in the various subsystems of the C-5. The Malfunction Detection Analysis and Recording System uses a digital computer to identify malfunctions in replaceable units. Failure and trend information is recorded on magnetic tape for analysis by maintenance people.
Crew Six (pilot, co-pilot, two flight engineers, two loadmasters)
Date Deployed December 1969 (for training); June 1970 (operational); December 1984 (to Reserve).
Inventory Active-force, 70; ANG, 11; Reserve, 28.
Cost C-5A, $163.4 million; C-5B, $167.7 million
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