Ensiklopedia Pesawat tempur

[eL'z]

masih kurang lengkap nih boss..
/heh/heh/heh/heh/heh

 

[locke cole]

pesawat tempurnya israel kok g ada yah --a

F-16I Sufa (Israel)​

Specifications
Weight 12.8 Tons (Empty)
23.5 Tons (Maximum)
Dimensions Length: 48' 10" (14.93 M)
Wingspan: 31' 0" (9.45 M)
Height: 16' 8" (5.1 M)
Propulsion Pratt & Whitney F100-PW-229
Thrust to Weigh Ratio: 8:1
Performance High Altitude: Over Mach 2
Low Altitude: 1440 KPH
Radius of Action: 2100 km
Combat Systems Missiles: Rafael Python 5, AMRAM (AIM-120)
Lightning Targetting
LANTIRN Navigation
JDAMs bomb

 

[legionsa]

tambah lagi dunk.. klo isa psawat yg di pake di BF2 ... ehehhee

 

[nuze]

@locke cole
klo psawat tempurnya israel...
dibiyayain ma amrik yah...?

 

[lardlles]

IZIN Tambahin Untuk VERSI klasik Aircraft ....
Boulton Paul P.82 Defiant

Specifications (Boulton Paul Defiant Mk II)
Type: Two Seat Night Fighter
Design: Boulton Paul Design Team
Manufacturer: Bolton Paul Aircraft, Wolverhampton.
Powerplant: (Mk II) One 1,280 hp (954 kW) Rolls-Royce Merlin XX inline piston engine. (Mk I) One 1,030 hp (768 kW) Rolls-Royce Merlin III Vee 12-cylinder piston engine.
Performance: Maximum speed 313 mph (504 km/h) at 19,000 ft (5790 m); cruising speed 260 mph (418 km/h); service ceiling 30,350 ft (9250 m); initial climb rate 1,900 ft (579 m) per minute.
Range: 465 miles (748 km) on internal fuel.
Weight:
(Mk II) Empty 6,282 lbs (2849 kg) with a maximum take-off weight of 8,424 lbs (3821 kg). (
Mk I) Empty 6,078 lbs (2757 kg) with a maximum take-off weight of 8,350 lbs (3787 kg).
Dimensions:
Span 39 ft 4 in (11.99 m);
length 35 ft 4 in (10.77 m);
height 11 ft 4 in (3.45 m);
wing area 250.0 sq ft (23.23 sq m).
Armament: Four 7.7 mm (0.303 in) Browning machine-guns in a hydraulically operated dorsal turret with 600 rounds per gun.
Variants: Boulton Paul P.82 Defiant (prototype),
Defiant F.Mk I, Defiant NF.Mk IA, Defiant Mk II, Defiant TT.MK I, Defiant TT.MK III.
Avionics: AI Mk IV or Mk VI radar, Mandrel jamming system.
History: First flight (prototype) 11 August 1937; (production Mk 1) 30 July 1939; first delivery December 1939.
Operators: RAF.

 

[lardlles]

AIrCraft WW II

Fairey Firefly

Specifications (Fairey Firefly AS.Mk 5)
Type: Two Seat Naval Reconnaissance Fighter / Anti Submarine Strike Aircraft
Design: Fairey Aviation Design Team
Manufacturer: The Fairey Aviation Company
Powerplant: (AS.Mk 5) One 2,250 hp (1678 kW) Rolls-Royce Griffon 74 12-cylinder Vee piston engine. (Mk I up to No 470) One 1,730 hp (1290 kW) Rolls-Royce Griffon IIB 12-cylinder Vee liquid-cooled; (from No 471) 1,990 hp (1485 kW) Griffon XII. (Mks 4-7) One 2,250 hp (1678 kW) Griffon 74 12-cylinder Vee piston engine.
Performance: (AS.Mk 5) Maximum speed 386 mph (618 km/h) at 14,000 ft (4265 m); cruising speed 220 mph (354 km/h); service ceiling 28,000 ft (8534 m). (Mk I) Maximum speed 316 mph (509km/h); initial climb rate 1,700 ft (518m) per minute; service ceiling 28,000 ft (8534 m). (Mk 4) Maximum speed 386 mph (618 km/h); initial climb rate 2,050 ft (625 m) per minute; service ceiling 31,000 ft (9450 m).
Range: (AS.Mk 5) 1300 miles (2092 km) on internal fuel. (Mk I) 580 miles (933 km) on internal fuel. (Mk 4) 760 miles (1223 km) on internal fuel.
Weight: (AS.Mk 5) Empty 9,674 lbs (4388 kg) with a maximum take-off weight of 16,096 lbs (7301 kg). (Mk I) Empty 9,750 lbs (4422 kg) with a maximum take-off weight of 14,020 lbs (6359 kg). (Mk 7) Empty 11,016 lbs (4997 kg) with a maximum take-off weight of 13,970 lbs (6337 kg).
Dimensions: (Mk 4 - 6) Span 41 ft 2 in (12.55 m); length 37 ft 11 in (8.51 m); height 14 ft 4 in (4.37 m); wing area 330.0 sq ft (30.66 sq m). (Mk I - III) Span 44 ft 6 in (13.55m); length 37 ft 7 in (11.4 m); height 13 ft 7 in (4.15 m).
Armament: (Mk I) Four fixed 20 mm Hispano cannon in wings and underwing racks for up to two 1,000 lbs (454 kg) of bombs or sixteen 60 lbs (27 kg) rocket projectiles. (Mk 4 and 5) usually similar to 1 in most sub-types. (Mk 6) no guns, but underwing load increased to 3,000 lbs (1362 kg) and varied. (Mk 7) no guns, but underwing load remained at 3,000 lbs (1362 kg) and equipment changed.
Variants: Firefly F.Mk 1, Firefly FR.Mk 1, Firefly F.Mk IA, Firefly NF.Mk 11, Firefly NF.Mk I, Firefly T.Mk 1, Firefly T.Mk 2, Firefly T.Mk 3, Firefly F.Mk III, Firefly F.Mk IV, Firefly FR.Mk 4, Firefly TT.Mk 4, Firefly Mk 5, Firefly Mk 6, Firefly FR.Mk 5, Firefly NF.Mk 5, Firefly AS.Mk 5, Firefly AS.Mk 6, Firefly TT.Mk 5, Firefly TT.Mk 6, Firefly, AS.Mk 7, Firefly T.Mk 7 ASW, Firefly U.Mk 8, Firefly U.Mk 9.
Avionics: AI Mk X radar, ASH Scanner, sonobuoys.
History: First flight 22 December 1941; first production F.1 26 August 1942; production FR.4. 25 May 1945; final delivery of new aircraft May 1955.
Operators:United Kingdom (RN), Canada (RCN), Australia.
Number Built: ~1533
----------------------------------------

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IZIN Tambahin Untuk VERSI klasik Aircraft ....
Gloster Gladiator

Specifications (Gloster Gladiator Mk II)
Type: Single Seat Biplane Fighter
Design: H.P. Folland
Manufacturer: Gloster Aircraft Company
Powerplant: (SS.37) One 645 hp (481 kW) Bristol Mercury VIS radial engine. (Mk I) One 840 hp (626 kW) Bristol Mercury IX or IXS 9-cylinder radial engine. (Mk II) One 830 hp (619 kW) Briston Mercury VIIIA 9-cylinder radial engine.
Performance: Maximum speed 253mph (407km/h); initial climb rate 2,300 ft (700 m) per minute; service ceiling 33,000 ft (10060 m).
Range: (Mk I and II) 440 miles (708 km); (Sea Gladiator) 425 miles (684 km).
Weight: (Mk I and II) Empty 3,450 lbs (1565 kg) with a maximum take-off weight of 4,750 lbs (2155 kg). (Sea Gladiator) Empty 3,745 lbs (1699 kg) with a maximum take-off weight of 5,420 lbs (2459 kg).
Dimensions: (Mk I and II) Span 32 ft 3 in (9.85 m); length 27 ft 5 in (8.38 m); height 10 ft 4 in (3.17 m).
Armament: First 71 aircraft, two 7.7 mm (0.303 in) Vickers machine guns in the fuselage, one 7.7 mm (0.303 in) Lewis machine gun under each lower wing; subsequent aircraft had four 7.7 mm (0.303 in) Browning machine guns in same locations. Fuselage guns had 600 rounds per gun and wing guns had 400 rounds per gun.
Variants: Gloster SS.37 (prototype), Gloster Gladiator, Gloster Gladiator Mk I, Gloster Gladiator Mk II, Gloster Sea Gladiator.
Avionics: None.
History: First flight (SS.37) September 1934; (Gladiator 1) June 1936; (Sea Gladiator) 1938; service delivery March 1 937; final delivery April 1 940.
Operators: Belgium, China, Egypt. Finland, Greece, Iraq, Ireland, Latvia, Lithuania, Norway, Portugal, South Africa, Sweden, UK (RAF, RN).

----------------
Gloster Meteor

Specifications (Gloster Meteor Mk I)
Type: Single Seat Fighter
Design: George Carter
Manufacturer: Gloster Aircraft Company
Powerplant: (Mk I) Two 1,700 lbs (771 kg) thrust Rolls-Royce W.2B/23C turbojet engines. (F.Mk 8) Two 3,600 lbs (1633 kg) thrust Derwent 8 turbojet engines.
Performance: Maximum speed 415 mph (668 km/h) at 10,000 ft (3050 m); service ceiling 40,000 ft (12190 m); initial climb rate 2,155 ft (657 m) per minute.
Range: 1000 miles (1610 km) on internal fuel.
Weight: Empty 8,140 lbs (3693 kg) with a maximum take-off weight of 13,795 lbs (6257 kg).
Dimensions: Span 43 ft 0 in (13.10 m); length 41 ft 4 in (12.6 m); height 13 ft 0 in (3.96 m); wing area 374.0 sq ft (34.74 sq m).
Armament: Four 20 mm Hispano cannon mounted in the nose.
Variants: Gloster Meteor (prototype), G41.A Meteor F.Mk 1 (first production), Meteor F.Mk II, Trent-Meteor (turboprop prototype), Meteor F.Mk III, Meteor F.Mk IV (later known as F.Mk 4), Meteor T.Mk 7 (trainer), Meteor F.Mk 8 (most produced variant), Meteor FR.Mk 9 (fighter-reconnaissance), Meteor PR.Mk 10 (high altitude reconnaissance), Meteor NF.Mk 11, Meteor NF.Mk 12, Meteor NF.Mk 13 (tropicalized), Meteor NF.Mk 14, Meteor U.Mk 15/16 (pilotless target aircraft), Meteor U.Mk 21 (pilotless target aircraft - Australia), Meteor TT.Mk 20 (target towing with the Royal Navy).
Avionics: (NF.Mk 11) SCR-720 AI Mk 10 radar, (NF.MK 14) American built APS-21 radar.
History: First flight (prototype) 5 March 1943; squadron delivery (F.1) 12 July 1944.
Operators: Belgium, China, Egypt. Finland, Greece, Iraq, Ireland, Latvia, Lithuania, Norway, Portugal, South Africa, Sweden, UK (RAF, RN).

---------------------
de Havilland Mosquito

Specifications (de Havilland D.H.98 Mosquito FB.Mk VI)
Type: Two Seat Fighter Bomber, Reconnaissance & Night Fighter
Design: de Havilland Design Team
Manufacturer: The de Havilland Aircraft Company, Hatfield and Leavesden, also built by Airspeed, Percival Aircraft and Standard Motors (Canley). Built by de Havilland Aircraft Pty, in Australia and de Havilland Aircraft of Canada.
Powerplant: (Mks II, III, IV and early Vs) Two 1,230 hp (918 kW) Rolls-Royce Merlin 21 engines. (Late FB.Mk VI) Two 1,635 hp (1219 kW) Rolls-Royce Merlin 25 engines. (Mk IX) Two 1,680 hp (1253 kW) Rolls-Royce Merlin 72 engines. (Mk XVI) Two 1,680 hp (1253 kW) Rolls-Royce Merlin 72 or 1,710 hp (1276 kW) Rolls-Royce Merlin 73/77 engines. (Mk 30) Two 1,710 hp (1276 kW) Rolls-Royce Merlin 76 engines. (Mk 33) Two 1,635 hp (1219 kW) Rolls-Royce Merlin 25 engines. (Mk 34/35/36) Two 1,690 hp (1260 kW) Rolls-Royce Merlin 113/114 engines. Many other variants had corresponding Merlins made by Packard.
Performance: Maximum speed 362 mph (583 km/h) at 5,500 ft (1675 m); maximum cruising speed 325 mph (523 km/h) at 15,000 ft (4570 m); service ceiling 33,000 ft (10060 m); initial climb rate of 1,870 ft per minute with a climb to 15,000 ft in 9 minutes 30 seconds.
Fuel: 453 Imp gal (544 US gal) plus provision for a 66.5 Imp gal (79.9 US gal) fuselage tank. (Externally) Up to 200 Imp gal (240 US gal) in 2 × 100 or 50 Imp gal (120 or 60 US gal) underwing droptanks.
Range: 1,650 miles (2655 km) with internal bombload.
Weight: Empty 14,300 lbs (6486 kg) with a loaded take-off weight of 22,300 lbs (10115 kg).
Dimensions: Span 54 ft 2 in (16.51 m); length 40 ft 10 3/4 in (12.47 m); height 15 ft 3 in (4.65 m); wing area 454 sq ft (42.18 sq m).
Armament: Four 20 mm Hispano Mk II cannon with 150 rounds per gun in the lower nose and four 7.7 mm (0.303 in) Browning Mk II machine-guns in the upper nose plus 2,000 lbs (907 kg) of bombs or 1,000 lbs (454 kg) of bombs and eight 60 lbs rocket projectiles.
History: First flight (prototype Mk I) 25 November 1940; first flight (NF.Mk II) 15 May 1941; first flight (T.Mk III) January 1942; first delivery (B.Mk IV) 105 Squadron at Swanton Morley in November 1941.
Operators: Austraila, Belguim, Canada (RCAF), China, Czechoslavakia, France, Yugoslavia, New Zealand, Norway, Soviet Union, Turkey, United Kingdom (RAF, RN, BOAC), United States (AAF).
Number Built: 7,781
Number Still Airworthy: One (Previously airworthy, but has not flown for the last few years.)
Nicknames: Mossie; Balsa Bomber; Wooden Wonder; Freeman's Folly (early nickname referring to Air Council member Sir Wilfred Freeman); Tsetse (Mk XVIII anti-shipping variant).

-----------------------------------------------------------------------
BOMBER VERSION

Handley Page Hampden

Specifications (Handley Page Hampden
Type: Four-Seat bomber (later torpedo bomber and minelayer).
Origin: Handley Page
Models: H.P. 52 Hampden I and H.P. 53 Hereford I
First Flight:
Prototype H.P. 52: June 31, 1936
Production Hampden I: May 1938
Production Hereford I: December 1939
Service Delivery: 1939
Production Halted: March 1942
Number Produced:
1,430 Hampdens (Handley Page 500, English Electric 770, Canadian Associated Aircraft 150)
100 Herefords were built by Short Brothers but failed to achieve operational status, many rebuilt as Hampdens.

Engine:
Hampden I

• Model: Bristol Pegasus XVIII
• Type: 9-Cylinder air cooled radial
• Number: Two Horsepower: 1,000 hp

Hereford I

• Model: Napier Dagger VIII
• Type: 24-Cylinder air cooled H-type
• Number: Two Horsepower: 1,000 hp

Dimensions:

• Wing span: 69 ft. 2 in. (21.98m)
• Length: 53 ft. 7 in. (16.33m)
• Height: 14 ft. 4 in. (4.37m)
• Wing Surface Area: N/A

Weights:
Empty:

• Hampden: 11,780 lb. (5344 kg)
• Hereford: 11,700 lb. (5308 kg)

Loaded:

• Hampden: 18,756 lb. (8508 kg)
• Hereford: 16,000 lb. (7257 kg)

Performance:
Maximum Speed:
Hampden: 254 mph (410 km/h)
Initial Climb: 980 ft/min (300 m/min)
Service Ceiling: 19,000 ft. (5790m)
Range (Fully loaded): 1,095 miles (1762 km)
Armament:
One .303 in. Vickers fixed forward.
One .303 in. Lewis manually aimed from nose by nav/bomb aimer.
One .303 in. Lewis manually aimed by wireless operator from upper rear position. One .303 in. Lewis manually aimed by lower rear gunner.
By January 1940 both rear positions refitted with twin Vickers and increased firing arcs.
Payload: 4,000 lb. (1814 kg.) of bombs internally.
By January 1940 hardpoints were added for two 500 lb. bombs added below outer wings, provision for carrying mines or one 18 in. torpedo
------------------------------------------------------------------
Avro Lancaster

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Specifications (Avro 683 Lancaster B.Mk I & III)

Type: Seven or Eight Seat Heavy Bomber

Accommodation/Crew: A crew of seven consisting of the Pilot, Flight Engineer, Observer/Nose Gunner/Bomb-aimer, Navigator, Radio/Wireless Operator, Mid-Upper Gunner, and Tail Gunner. The Bomb-aimer was in the nose position below the front turret. Above and behind and to the port is the Pilot's position in a raised canopy with good all-round vision and armour plating on the back of the seat and armour protection behind his head. Inside the canopy immediately aft of the pilot's seat is the Fighting Controller's position and is provided with special bullet-proof glass. Slightly aft of this position is the Navigator's position, with table, chart stowage and astral done in the roof. At the rear end of the navigator's table and just forward of the front spar is the Radio Operator's station. Within the centre-section is a restroom with a bed. Aft of the rear spar is the mid-upper and mid-lower turrets, together with various equipment stowage for flares, emergency rations, etc. A dinghy is carried in the centre-section trailing-edge portion of the wing and is automatically deployed and inflated upon impact with water. It can also be operated by hand. In the extreme tail is the rear turret. A walkway is provided along the entire length of the fuselage and the main entrance door is situated on the starboard side just forward of the tailplane.

Design: Chief Designer Roy Chadwick and Managing Director Roy Dobson of A. V. Roe Aircraft Company Limited based on the Avro 679 Manchester design

Manufacturer: Alexander V. Roe (Avro) Aircraft Company Limited based in Greengate, Middleton (Chadderton), Manchester with another production facility located at Yeadon. Prior to 1938, the main plant was located in Newton Heath, but in the spring of 1939 the company moved its main office to the new, much larger facility in Greengate. In order to further expand production capability, Metropolitan Vickers Limited of Trafford Park (Manchester), Armstrong Whitworth Limited of Baginton and Bitteswell (Coventry), Austin Motors of Longbridge (Birmingham), Vickers Armstrong of Chester and Castle Bromwich and Victory Aircraft of Canada (Malton, Ontario) also built the aircraft. A large number of sub-contractors were also involved in component manufacture.

Powerplant: (B.Mk I) Initially four Rolls-Royce Merlin XX or 22 Vee 12-cylinder liquid-cooled inline engines each rated at 1,280 hp (955 kW) for take-off and 1,240 hp (925 kW) at 2,850 rpm at 10,000 ft (3050 m) with a maximum power rating of 1,480 hp (1104 kW) at 3,000 rpm at 6,000 ft (1830 m). Late production B.Mk I aircraft being equipped with four Rolls-Royce Merlin 24 Vee 12-cylinder liquid-cooled inline engines rated at 1,620 hp (1209 kW) for take-off and 1,240 hp (925 kW) at 2,850 rpm at 10,000 ft (3050 m) with a maximum power rating of 1,640 hp (1223 kW) at 3,000 rpm at 2,000 ft (610 m). (B.Mk II) Four Bristol Hercules VI 14-cylinder two-row air-cooled radial engines rated at 1,615 hp (1205 kW) for take-off and 1,675 hp (1250 kW) at 2,900 rpm at 4,500 ft (1370 m) with a maximum power rating of 1,675 hp (1250 kW) at 2,900 rpm at 4,500 ft (1450 m). The radial engined Lancasters had a higher top speed but also had a higher fuel consumption. (B.Mk III) Four American-built Packard Merlin 28 Vee 12-cylinder liquid-cooled inline engines each rated at 1,300 hp (970 kW) for take-off, or four American-built Packard Merlin 38 (Merlin 22) Vee 12-cylinder liquid-cooled inline engines each rated at 1,390 hp (1037 kW) for take-off. Some later B.Mk III aircraft had the American-built Packard Merlin 224 (Merlin 24) Vee 12-cylinder liquid-cooled inline engines each rated at 1,620 hp (1209 kW) for take-off. All Merlin engines used a mechanically driven, two-speed, single stage, centrifugal supercharger. Note: Rolls-Royce engine marks up to XX (twenty) are distinguished by Roman numbers, while marks above that were distinguished by Arabic numericals.

Propellers: Hamilton-Standard or Rotol propellers. In later aircraft paddle-bladed Nash-Kelvinator propellers were used increasing the cruising speed by 8 mph (12.9 km/h) and the service ceiling by 1,500 ft (457 m). The airscrew shaft was a SBAC No. 5 type with a reduction gear ratio of 0.42:1.

Performance: (Early B.Mk I) Maximum speed 275 mph (443 km/h) at 15,000 ft (4572 m). (Late B.Mk I) Maximum speed 287 mph (462 km/h) at 11,500 ft (3505 m), 275 mph (443 km/h) at 15,000 ft (4572 m), 260 mph (419 km/h) at 19,400 ft (5913 m); cruising speed 234 mph (377 km/h) at 21,000 ft (6401 m), 200 mph (322 km/h) at 15,000 ft (4572 m); stalling speed (clean) 95 mph (153 km/h) at 60,000 lbs (27211 kg); normal service ceiling 23,000 ft (7010 m), nominal service ceiling 24,500 ft (7468 m); absolute service ceiling 24,671 ft (7500 m); climb to 20,000 ft (6096 m) in 41 minutes and 40 seconds; initial rate of climb 250 ft (76 m) per minute with full bombload. In a hard dive the prototype aircraft achieved speeds reaching almost 400 mph (644 km/h) with production aircraft (operational loadout) being limited to 360 mph (578 km/h).

Carburetion (Merlin): SU float carburettor, type AVT 40 / 241 / 216 / 224 / 227. American built Packard Merlins had the Bendix Stromberg pressure-injected type.

Ignition (Merlin): Two BTH C.5 SE12-S or Rotax NSE12-4 magnetos.

Fuel Capacity / Specification: A total of six fuel tanks consisting of two 580 Imperial gallon (703 US gallon or 2637 litre) inboard tanks, two 383 Imperial gallon (464 US gallon or 1740 litre) intermediate tanks and two 114 Imperial gallon (138 US gallon or 518 litre) outboard tanks giving the aircraft a total fuel capacity of 2,154 Imperial gallons (2,610.6 US gallons or 9790 litres). Provisions for one or two overload fuel tanks of 400 Imperial gallons (485 US gallons or 1818 litres) each could be carried in the bomb bay. Fuel specification 100 / 130 Grade DED 2475 (AN-F-28).

Coolant Capacity / Specification: 5 Imperial gallons (6 US gallons or 22.7 litres) per engine made up of 70 percent water + 30 percent ethylene glycol to specification DTD 344 A.

Oil Capacity / Specification: Each engine had its own oil tank in the nacelle with a capacity of 37.5 Imperial gallons (45.4 US gallons or 170.25 litres) for a total of 150 Imperial gallons (181.6 US gallons or 681 litres). Oil specification DED 2472 / B / O.

Range (typical): 2,530 miles (4072 km) with a bombload of 7,000 lbs (1795 kg); 1,730 miles (2786 km) with a bombload of 12,000 lbs (5442 km); 1,550 miles with a bombload of 22,000 lbs (9977 kg).

Weights & Loadings: Empty (clean) 39,600 lbs (16740 kg), empty (equipped) 53,300 lbs (24040 kg) with a maximum take-off weight of 65,000 lbs (29480 kg). The B.Mk I Special had a maximum take-off weight of 70,000 lbs (31751 kg) while carrying a 22,000 lbs (9980 kg) Grand Slam bomb. Wing loading 52.7 lbs/sq ft (258 kg/sq m); power loading 13.3 lbs/hp (6.35 kg/hp).

Dimensions: Span 102 ft 0 in (31.09 m); length 69 ft 6 in (21.18 m); height 20 ft 6 in (6.25 m); wing area 1,297.0 sq ft (120.49 sq m); tailplane area: 237.0 sq.ft (22.0 sq m); tail fin and rudder area: 111.40 sq ft (10.35 sq m); aileron span 17 ft 3 in (5.3 m).

Gunsights: The main gunsight used in Lancaster turrets was the Barr & Stroud G Mk Ill reflector sight. In use the screen was mounted at a 45 degree angle showed an illuminated orange circle with a central dot, both focused at infinity. A brightness control adjusted it according to conditions; bright in sunlight, dim at night. The radius of the circle was approximately equal to the wingspan of a single-engined fighter at a range of 1,200 ft (365 m), while the radius of the circle gave the deflection (the amount of aiming ahead) needed to hit a target with a relative crossing speed of 50 mph (80 km/h). In 1944, the Mk llc gyroscopic sight entered service as a turret sight. This could actually predict the point of aim, if the approaching fighter could be tracked for a short while, and its wingspan set on a dial.

Defensive Armament: A total of ten 7.7 mm (0.303 in) Browning machine-guns in a nose, mid-upper, tail and ventral position. The ventral position was soon deleted on most RAF Lancasters as it was thought unnecessary and took the same position as the H2S radome. Where possible, and unofficially, many crews installed a single 7.7 mm (0.303 in) or 12.7 mm (0.50 in) Browning machine-gun on aircraft lacking the ventral turret in order to deal with the ever increasing 'behind and below' attacks of German night fighters using Schräge Musik, which interesting, did not use tracer ammunition. These were hastily installed configurations usually consisting of the gunner sitting on a bicycle type seat with the ammunition box being bolted to the floor and the gun mounted in a hole cut into the floor. The British would eventually re-introduce the F.N.64 turret on aircraft equipped with G-H radar (an improved version of Gee) since that type of radar did not have the large radome as the H2S required. During 1943/1944 when the use of Schräge Musik on german Nachtjagd (night fighters) became widespread, the new twin-gun F.N.64 power-operated turrets became the most important gun position on the bomber. On aircraft that were modified to carry the "Tall Boy" or "Grand Slam" bombs, most had the nose and mid-upper turrets were removed and the tail turret reduced to a single pair of 7.7 mm (0.303 in) Browning machine-guns in order to reduce weight. The 7.7 mm (0.303 in) ammo consisted of Ball, Tracer, Armour Piercing and Incendiary.

• 2 × 7.7 mm (0.303 in) Browning Mk II trainable forward-firing machine-guns in the power-operated Frazer-Nash F.N.5A nose turret with 1,000 rounds per gun using a Barr & Stroud G Mk III reflector sight
  
• 2 × 7.7 mm (0.303 in) Browning Mk II trainable machine-guns in the power-operated Frazer-Nash F.N.50 (Boulton-Paul) dorsal turret with 1,000 rounds per gun using a Barr & Stroud G Mk IIIA reflector sight.
• 4 × 7.7 mm (0.303 in) Browning Mk II trainable rearward-firing machine-guns in the power-operated Frazer-Nash F.N.20A tail turret with 2,500 rounds per gun using a Barr & Stroud G Mk III reflector or Gyro Mk IIc sight.
  
• 2 x 7.7 mm (0.303 in) Browning Mk II trainable rearward firing machine-guns in a power-operated Frazer-Nash F.N.64 ventral turret with 500 rounds per gun using a periscopic sight. (This position did not have a dedicated gunner).

Offensive Ordnance: Up to 8,000 lbs (3629 kg) of bombs carried in a 33 ft (10.0 m) long under fuselage internal bomb bay. While capable of carrying much more weight, early aircraft were limited to 8 x 1,000 lbs (454 kg) GP/MC (General Purpose Medium Capacity) bombs due to the physical restrictions of the bomb bay, but continued improvements enabled later production aircraft to carry up to 14,000 lbs (6350 kg) of bombs normally, including 2,000 lbs (907 kg) AP (Armour Piercing) or HE/SAP (High Explosive Semi-Armour Piercing) bombs, 4,000 lbs (1814 kg) HE/HC (High Explosive High Capacity) 'Block Buster' (also called a "Cookie") and a single 8,000 lbs (3628 kg) HE/HC (High Explosive High Capacity) bomb. Some aircraft underwent special modifications to allow them to carry the 12,000 lbs (5443 kg) HE/DP (High Explosive Deep Penetration) 'Tall Boy', the 12,000 lbs (5443 kg) HE/HC (High Explosive High Capacity) 'Factory Buster' and the 22,000 lbs (9979 kg) HE/DP (High Explosive Deep Penetration) 'Grand Slam' bombs. The 12,000 lbs (5443 kg) HE/HC 'Factory Buster' was actually three 4,000 lbs (1800 kg) HC High Explosive "Cookies" bolted together given the bomb a total of 5,200 lbs (2358.7 kg) of Torpex 'cemented' within a 1 inch (25.4 mm) jacket of TNT. Aircraft capable of carrying the larger 4,000 lbs (1800 kg) and 8,000 lbs (3629 kg) bombs can easily be identified by the use of a bulged bomb bay door.
Standard loadouts were as follows:

• -Blast & Demolition - 1 x 8,000 lbs (3628 kg) HE plus up to 6 x 500 lbs (227 kg) HE bombs.
• -Blast & Demolition - 14 x 1,000 lbs (454 kg) bombs.
• -Blast, Demolition & Fire - 1 x 4,000 lbs (1814 kg) HE 'Cookie' plus 3 x 1,000 lbs (454 kg) HE bombs plus up to 6 SBC (Small Bomb Cannisters) each holding either 236 x 4 lbs (1.8 kg) or 24 x 30 lbs (13.6 kg) incendiaries.
• -Blast, Demolition & Fire - 1 x 4,000 lbs (1814 kg) HE 'Cookie' plus up to 12 SBC (Small Bomb Cannisters) each holding either 236 x 4 lbs (1.8 kg) or 24 x 30 lbs (13.6 kg) incendiaries.
• -Maximum incendiary - 14 SBC (Small Bomb Cannisters) each holding either 236 x 4 lbs (1.8 kg) or 24 x 30 lbs (13.6 kg) incendiaries.
• -Deployed Tactical Target - 1 x 4,000 lbs (1814 kg) HE 'Cookie' plus up to 18 x 500 lbs (227 kg) HE bombs.
• -Low Level Attack - 6 x 1,000 lbs (454 kg) HE bombs with delayed action fuses.
• Hardened Targets & Ships - 6 x 2,000 lbs (907 kg) AP bombs with very short fuses.
• -Mine Laying - Up to 6 x 1,500 lbs (680 kg) or 1,850 lbs (839 kg) parachute sea mines which could be either acoustic or magnetic. First used on the night of 3/4 March 1942.

Variants: BT308 (first prototype), DG595 (second prototype), B.Mk I, B.Mk I Special (Grand Slam), B.Mk I FE (Far East), B.Mk II (Hercules engines), B.Mk III, B.Mk III Type 464 Special (Dambuster), B.Mk IV (renamed Lincoln Mk I), B.Mk V (renamed Lincoln Mk II), B.Mk VI, B.Mk VII, B.Mk VIII FE (Far East), B.Mk X (Canadian Built).

Equipment/Avionics: The Mark IXA Course-Setting Bomb Sight (CSBS) and the Mark XIV Computing Bomb Sight (CBS) were standard. The Radio section is complete with a Marconi Transmitter T.1154 and Receiver R.1155 with a Morse key on the right of the wireless operators table. The operator was also provided with a switching gear to connect crew positions to the receiver or transmitter if required. H2S "Fishpond" Indicator 182 aircraft detection display plus all the auxiliary equipment. The Navigators section contains the Gee & Oboe radio guidance navigation equipment, H2S main blind bombing/mapping radar with the PPI (Plan Position Indicator) plus all the navigation aids used prior to the introduction of the Gee, Oboe & H2S radars. An improved H2X radar would replace the older H2S radar after German FuG 350 Naxos Z radar equipped night fighters could home in on the H2S radar transmissions. Some aircraft used the "Monica" tail mounted early warning radar which was effective to a range of about 1,000 yards, but had no IFF (Identification Friend or Foe) capability. Monica was discontinued in use when it was discovered that German FuG 227 Flensburg radar equipped night fighters could actually home in on the transmission signal given out by the Monica radar. Rebecca navigation radar was also used on small numbers of aircraft. Boozer early warning radar (ground and air) was also used and considered better than Monica. Tinsel was an electronic warfare jamming device which in its early use was successful, but German response to the device limited later effectiveness. An automatic gun-laying apparatus (A.G.L.T) code-named 'Village Inn' was fitted to the F.N.121 tail turret to allow radar guided beyond visual range firing. The device although potentially devastating, it originally lacked the ability to distinguish between Friend or Foe. The aircraft is also fully equipped for night flying. An F.24 camera was standard equipment for vertical photography to confirm bombing accuracy.

________________________________________________________

Berbagi Ilmu dengan BErbagi Info​

 

[Roc-A-Fella]

Req f-35

Cuman pingin tahu F-35
Abis liat trailernya Tom Clancy's H.A.W.X

Keren abis, and pesawatnya keliatan real banget

Sembari menunggu releasenya, fall 2009

Thanks before

 

[honeyproot]

bro, setau gue yg di trailer H.A.W.X. itu adalah pesawat Rafale, buatan Prancis. Kalo F-35 itu muncul di film Die Hard 4, yang nembakin bruce willis pas lagi naek truk.

 

[khoe]

wow panjang bgt kk....

gw jg sukayg f-35

 

[aceng ms]

mantep2 bner pesawat tempur jadi pingin tuh coba naik....
we....

 

[nzw]

sukhoi yang punya indonesia mana?

 

[phonx]

Pesawat tempur Sovyet kok dikit yah?

 

[crocodylus]

pesawat siluman tu gan

 

[animenaruto1]

still may favorit is f14 tom cat

 

[manful]

emang gile banget negara pamansam ini ya, dalam segala hal mereka unggul.....*salut*

 

[Bledeg]

raptor kalo di film ironman bikinan tony stark loh hihihi

 

[suto1979]

Bagus keren

 

[biro ijazah asli]

Nice info