Thursday, July 12, 2007

E-3




GENERAL DATA

Country of Origin. USA.
Similar Aircraft. A-50 Mainstay.
Crew. Seventeen.
Role. AWACS.
Armament. None.
Dimensions. Length: 152 ft, 9 in (46.6 m). Span: 154 ft, 7 in (44.4 m).

WEFT DESCRIPTION :

Wings. Low-mounted, swept-back, and tapered with a positive slant. An electronics pod is mounted on the right wing-tip.
Engine(s). Four turbojets mounted on pylons under the wings. Engines extend well forward of the wings’leading edges.
Fuselage. Round, cigar-shaped, tapers to the rear. Rounded nose, stepped-up cockpit. Large radome on top of the body between the wings and tail section.
Tail. Swept-back, tapered fin with a square tip. Flats are swept-back, tapered, and mid-mounted on the fuselage.

USER COUNTRIES : Israel, Luxembourg (NATO), Saudi Arabia, USA.

The radar dome on the back is the most special part of the E-3 to other aircrafts in appearance. It is 30 feet (9.1 meters) in diameter, six feet (1.8 meters) thick, and held 11 feet (3.3 meters) above the fuselage by two struts. It contains a radar subsystem that permits surveillance from the Earth's surface up into the stratosphere, over land or water. The detect range is more than 200 miles (320 kilometers) for low-flying targets and farther for medium to high altitudes. An identification friend or foe subsystem of the radar can look down to detect, identify and track enemy and friendly low-flying aircraft by eliminating ground clutter returns. In this situation, other types of radars may be confused. The unit cost of the E-3 is approximately $270 million, which is greatly effected by the high price eletronic equipment onboard.

The variations of E-3 include E-3A, E-3B, E-3C and E-3D. The A type is the first production version for US airforce. A type`s inside is quite different from the prototype, the modified fuselage can hold 17 people. They are 4 pilots, 12 operators and 1 onboard officer. The operators will charge the communication, computer, radar and 9 multi-function display plat. The equipment can be devided into six parts which are radar, IFF, data processing, communication, navigation, data display and control. The radar system includes the Northrop Grumman AN/APY-1 radar, the multi function of the radar can seperate the whole 360 degree area into 32 parts and use different function in each part. Scan once, the IFF system can check over 200 targets with IFF receiver installed, no matter the target is in the air, on the ground or sea.

There are some other major subsystems in the E-3, navigation, communications and computers (data processing). The navigation subsystem can offer a total positioning deflection less than 3.7km. The data display and control system is mainly formed of data display, multi-function control plat, eletronic typewriter and assis-display. The data can be showed in original size or zoom to 32 times bigger, the latter is for detect and control fighters to proceed dog-fight mission. The data processing system can record, save and operate the data from the radar, IFF, navigation and other equipment in the aircraft. The system can process 400 targets or 600 for european variations. The operators onboard will look at the consoles display computer-processed data in graphic and tabular format on video screens to check all the information. And the operators will perform surveillance, identification, weapons control, battle management and communications functions

The E-3 can gather and present broad and detailed battlefield information for different military units in real time, which includes position and tracking information on enemy aircraft and ships, and location and status of friendly aircraft and naval vessels. In time of crisis, such as Nuclear strike, this data can be forwarded to the National Command Authorities in the United States.

As an aircraft, the Sentry has an excellent chance of surviving in war. The flight path can quickly be changed according to mission and survival requirements. The E-3 can fly a mission profile for more than 8 hours, or much longer through inflight refueling.

The aircraft can be used as a surveillance asset in support of other government agencies during counter drug operations. U.S. Customs Service officers may fly aboard the E-3 Sentry on precoordinated missions to detect smuggling activities.

There are four E-3 Sentries in Pacific Air Forces assigned to the 961st Airborne Air Control Squadron (AACS), based in Japan, and the 962nd AACS, Elmendorf AFB, Alaska.

E-3“望楼”空中预警机The E-3B is developed from the first two E-3s, the target processing and ship detecting ability is strengthened. The E-3C and E-3D is designed for NATO and UK which is close to B type. NATO airforces have acquired 18 of the aircraft and support equipment for US$ 2 billion. The first E-3 was delivered to NATO in January 1982. The Peace Sentinel program for Saudi Arabia began in 1981. It included five AWACS aircraft and six E-3 derivative (KE-3) inflight refueling tanker aircraft, along with spare parts, trainers and support equipment. In 1984, the Saudi government exercised an option to increase the tanker order to eight. The United Kingdom ordered six E-3s in 1987 after some frustrations, US$ 260 million each, later order for one more E-3 added on. And France ordered 3(photo up here) for US$ 330 million each, deployed between 1989 to 1992, as well as one added on, too.


E-3“望楼”空中预警机

E-3 Sentry were among the first to deploy during Operation Desert Shield. During Desert Storm, E-3s flew more than 400 missions and logged more than 5,000 hours of on-station time. The E-3 controllers assisted in 38 of the 40 air-to-air kills recorded during the conflict.

Experience has proven that the E-3 Sentry can respond quickly and effectively to a crisis and support worldwide military deployment operations.

Improvement program for the E-3 began with a U.S. Air Force award of the ICON (Integration Contract) to Boeing in May 1987. ICON will equip both U.S. and NATO E-3s with an electronic support measures (ESM) passive surveillance capability, and other enhancements to the U.S. E-3 fleet.

In 1989, the US airforce received the first 7 E-3s with the Boeing "Radar system improvement project RSIP" rebuilt. RSIP updates the pulse Doppler radar`s sensitivity and counter-countermeasures ability, as well as the GPS added on. And the radar operators console is updated, replaced the radars existing computer with a new high-reliability multiprocessor and rewrite the radar software to make it easier to maintain and enhance in the future. The Northrop Grumman offered the radar computer, radar control maintain interface and other hardware in this project. The whole project is completed after the NATO and UK E-3s got the same updates in 1996.

Tuesday, June 12, 2007

Hawker Siddley Buccaneer




Manufacturer : Blackburn/Hawker-Siddeley Aviation/British Aerospace
designer : Blackburn
Use :Aanvals and patrols plane
Engine : (S.1) 2 x bristol Siddeley Gyron junior 101, later versions all 2 x Rolls-Royce Spey 101
Capacity : 3220 kilogrammes (BS.101), 5003 kilogrammes (Rolls-Royce Spey 101) attachment amplitude : (S.1) 12.9 m., (later versions) 13.41 m. length 19.33 m. altitude 4.95 m. wing surface Klimvermogen 2134 m./charged minus weight empty 11,800 kilogrammes (S.1), 13,610 kilogrammes (later versions) 20,865 kilogrammes (S.1), 28,123 kilogrammes (later versions)
speed maximum. 1038 km/u (sea altitude) charged ceiling 12,200 m. range 3700 km with weapon charge arms rotating bomb shutter 4 x 454 kilogrammes boom or exploration pot or 2000 litres fuel, celebrate ophangpunten for several weapons, totally weapon charge 7257 kilogrammes
crew : 2
first escapes : 30 April 1958
numbers built : 170

convair B 58




Manufacturer : Convair
Designer
Use : Strategic supersone nuclear and conventional bomber
Engine : 4 x General Electric J79-GE-1 turbojets.
Capacity 7057 kilogrammes with naverbrander charged by engine attachment amplitude 17.32 m.
length 29,49m
altitudes 9.58 m.
wing surface 470 m²
Klimvermogen
weight empty 25,201 kilogrammes 73,935 kilogrammes
speed maximum. 2125 km/u charged on 19,248 m.
altitude 1850 km, ceiling 19,248 m. (record altitude; 26,017 m) range 2816 km, with inflight refueling; 8975 km arms 20mm Vulcan gun in the tail, nuclear or conventional booms in large romppod or under the wings.
Crew 3
First escapes 11 November 1956
Numbers built 148

Friday, May 18, 2007

Sukhoi S-32/37








Country of origin: Russia

Type: Fighter technology demonstrator

Powerplants: Two 152kN (34,200lb) with afterburning Aviadvigatel D-30F6 turbofans. May latter be fitted with two 196kN (44,000lb) with afterburning and thrust vectoring Saturn AL-31 F turbofans.

Performance: Max speed at 30,000ft 2200km/h (11 190kt), max speed at sea level 1400km/h (756km/h). Service ceiling 59,000ft. Basic range 3300krn (1 782nm).

Weights: Normal takeoff 25,670kg (56,590lb), max takeoff 34,000kg (74,690lb).

Dimensions: Wing span 16.7m (54.7ft), length 22.6m (74ft), height 6.4m (21 ft).

Accommodation: Pilot only

Armament: None in the prototype. A production version would carry air-to-air and air-to-ground weapons in internal weapons bays and on external pylons.

Operators: Experimental aircraft, not in operational service.

Sukhoi Su27 Flanker




Airplane: Sukhoi Su27 Flanker
Type: Air superiority fighter
Technical data: Airplanes decay. Airplanes historically. Tanks decay.
- Engine: two Lyulka AL31F of jet engines Tank historically.
- Weapons: a 30mm cannon, ten external Pylone for a load to 6000kg
- Weight: Takeoff weight 30000kg
- Dimension: Span 14,70m, length 21,94m, height of 6,36m
- Achievement: 2500 kmh, service ceiling of 18000m, operation radius 1500 km Sports car. -

Picture: Sukhoi Su27 Flanker

Sunday, May 6, 2007

Saab Viggen





The Saab Viggen (Thunderbolt) is a Swedish fighter aircraft


General characteristics

  • Crew: One
  • Length: 53 ft 9 in (16.4 m)
  • Wingspan: 34 ft 9 in (10.6 m)
  • Height: 19 ft 4 in (5.9 m)
  • Wing area: 500 ft² (46 m²)
  • Empty weight: 26,900 lb (12,200 kg)
  • Loaded weight: lb (kg)
  • Max takeoff weight: 44,000 lb (20,000 kg)
  • Powerplant:Volvo RM8B afterburning turbofan, 16,200 lbf dry, 28,110 lbf afterburning (72.1 kN / 125.0 kN)

Performance

Armament

B-1 Lancer





The B-1 Lancer is an American long-range strategic bomber. The B-1B version has been in service with the United States Air Force (USAF) since 1986. Together with the B-52 Stratofortress and the B-2 Spirit, it is the backbone of the United States's long-range bomber force.

Specifications (B-1B)

B-1B orthographic projection.

General characteristics

  • Crew: 4: aircraft commander, copilot, offensive systems officer and defensive systems officer
  • Length: 146 ft (44.5 m)
  • Wingspan:
    • Extended: 137 ft (41.8 m)
    • Swept: 79 ft (24.1 m)
  • Height: 34 ft (10.4 m)
  • Wing area: 1,950 ft² (181.2 m²)
  • Airfoil: NA69-190-2
  • Empty weight: 192,000 lb (87,100 kg)
  • Loaded weight: 326,000 lb (148,000 kg)
  • Max takeoff weight: 477,000 lb (216,400 kg)
  • Powerplant:General Electric F101-GE-102 augmented turbofans
    • Dry thrust: 14,600 lbf (64.9 kN) each
    • Thrust with afterburner: 30,780 lbf (136.92 kN) each

Performance

Armament

Panavia Tornado





The Panavia Tornado is a family of twin-engine fighters, which was jointly developed by the United Kingdom, Germany and Italy. There are three primary versions of the Tornado, the fighter-bomber Tornado IDS (Interdictor/Strike), the interceptor Tornado ADV (Air Defence Variant), and the suppression of enemy air defences Tornado ECR (Electronic Combat/Reconnaissance).

Developed and built by Panavia, a trination consortium consisting of British Aerospace (then the British Aircraft Corporation), MBB of Germany, and Alenia Aeronautica of Italy, the Tornado first flew on August 14, 1974, and saw action with the RAF and AMI (Italian Air Force) in Operation Granby / Gulf War. International co-operation continued after its entry into service within the Tri-National Tornado Training Establishment, a tri-nation training and evaluation unit operating from RAF Cottesmore in Rutland in the English Midlands. Including all variants, 992 aircraft were built for the three partner nations and Saudi Arabia. Though still in service, plans are currently underway to replace the aircraft.


Panavia Tornado

Royal Air Force Panavia Tornado Royal Air Force Panavia Tornado GR1 carrying code DE on its tail is equipped with a laser guided bomb. It is powered by two afterburning Turbo Union RB199-103 turbofans of 15,800lb thrust.

Visit the RAF web page describing the Panavia Tornado GR1.

Royal Air Force Panavia Tornado Royal Air Force Panavia Tornado F3. It is powered by two afterburning Turbo Union RB199-34R Mk 104 turbofans of 16,520lb thrust.

Visit the RAF web page describing the Panavia Tornado F3.

Royal Air Force Panavia Tornado Royal Air Force Panavia Tornado F3 ZG757.

Specifications (Tornado IDS GR.4)

Orthographically projected diagram of the .
From upper left, lold livery of 6° Stormo, 50° Stormo, 36° Stormo, and livery used by 50° Stormo during operation Desert Storm.

General characteristics

  • Crew: 2
  • Length: 16.72 m (54 ft 10 in)
  • Wingspan: 13.91 m at 25° wing sweep, 8.60 m at 67° wing sweep (45.6 ft / 28.2 ft)
  • Height: 5.95 m (19.5 ft)
  • Wing area: 26.6 m² (286 ft²)
  • Empty weight: 13,890 kg (31,620lb)
  • Max takeoff weight: 28,000 kg (61,700 lb)
  • Powerplant:Turbo-Union RB199-34R Mk 103 afterburning turbofans, 43.8 kN dry, 76.8 kN afterburning (9,850 lbf / 17,270 lbf) each

Performance

Armament

  • 2x 27 mm Mauser BK-27 cannon with 180 rounds each
  • Four fuselage pylons and four swivelling underwing pylons for a maximum of 9000 kg (19,800 lb) of weapons, fuel, and ECM pods, inner wing pylons have shoulder rails for two AIM-9 Sidewinder or ASRAAM self-defence missiles. A wide variety of air-to-ground weapons can be carried including Wasp ASM, Kormoran anti-ship missiles, BAe Sea Eagle anti-ship missiles, AGM-65 Maverick ASM, BAe ALARM anti-radiation missile, LAU-51A and LR-25 rocket pods, napalm bombs, retarded bombs, BL755 cluster bombs, and Paveway series laser-guided bombs, MW-1 munitions dispenser, JP233 munitions dispenser, Storm Shadow, Brimstone, Taurus missile, can be equipped to carry B61 and WE.177 nuclear bombs.
  • RAPTOR Reconnaissance pod, TIALD laser designator
  • Rafael Lightening III targeting pod has replaced TIALD 500 during the UK RAF's operations in Iraq.

[edit] Tornado ADV F3

The ADV is in most respects similar to the IDS. It has been stretched (to 18.7 m) so as to accommodate the staggered quartet of BAe Skyflash missiles. It includes just one internal Mauser cannon rather than the two of the original IDS (the GR4 only has 1 cannon). The ADV uses the Turbo-Union RB199-34R Mk 104. It has an empty weight of 14,500 kg, and has different weapons stores from the IDS (suiting its interceptor role).

B2 Spirit Bomber


The Northrop Grumman B-2 Spirit is a multi-role stealth bomber able to drop conventional and nuclear weapons. The bomber development was a milestone in the bomber modernization program of the U.S. Department of Defense.

The B-2's stealth technology is intended to help the craft penetrate defenses previously impenetrable by combat aircraft. The original procurement of 135 aircraft was later reduced to 75 in the late 1980s. In his 1992 State of the Union address, President George H. W. Bush announced total B-2 production would be limited to 20 aircraft (later increased to 21 by refurbishing a test aircraft).[1] This reduction was largely a result of the disintegration of the Soviet Union, which effectively rendered void the Spirit's primary mission.

The B-2 is one of the most expensive planes ever built: estimates for the costs per plane range from 1.157 billion[2] to 2.2 billion US dollars.[3] By comparison, a Nimitz class aircraft carrier costs $4.5 billion. However, quoted cost figures are highly inflated by the inclusion of the aircraft's enormous development cost and infrastructure development costs in the unit price; published estimates have shown the unit "production" cost for the aircraft alone is approximately $150 million per aircraft.

Specifications (B-2A Block 30)

Orthographically projected diagram of the B-2 Spirit

General characteristics

  • Crew: 2
  • Length: 69 ft (20.9 m)
  • Wingspan: 172 ft (52.12 m)
  • Height: 17 ft (5.1 m)
  • Wing area: 5,000 ft² (460 m²)
  • Empty weight: 158,000 lb (71,700 kg)
  • Loaded weight: 336,500 lb (152,600 kg)
  • Max takeoff weight: 376,000 lb (171,000 kg)
  • Powerplant:General Electric F118-GE-100 turbofans, 17,300 lbf (77 kN) each

Performance

Armament

  • 40,000 lb (18,000 kg) of Bomb Rack Assembly mounted 500 lb class bombs (Mk82) (total carriage quantity: 80)
  • 27,000 lb (12,000 kg) of BRA mounted 750 lb CBU class bombs (total carriage quantity: 36)
  • 16 Rotary Launcher Assembly (RLA) mounted 2000 lb class weapons (Mk84, JDAM-84, JDAM-102)
  • 16 RLA mounted B61 or B83 nuclear weapons

Later avionics and equipment improvements allow B-2A to carry JSOW and GBU-28s as well. The Spirit is also designated as a delivery aircraft for the AGM-158 JASSM when the missile enters service.

North American F86 Sabre




The North American F-86 Sabre (sometimes called the Sabrejet) was a transonic combat aircraft developed for the US Air Force. The F-86 was developed in the 1940s following the end of World War II and was one of the most-produced western jet fighters in the Cold War era

Specifications (F-86F)

Orthographically projected diagram of the F-86 Sabre.

Data from Quest for Performance[35]

General characteristics

Performance

Armament

  • Guns: 6× 0.50 in (12.7 mm) machine guns

Wednesday, April 25, 2007

MIG 29





Specifications MIG 29 Fulcrum:
Crew: one
Armament (internal): 30mm MK

Armament (optional): AA-8 (R-60) AA-10 C (R-27) AA-10 B (R-27) AA-11 (R-73) AS-12 (Kh-25M/Kh-27) AS-14 (Kh-29)
Bombs Rockets
Ammunition: 7 interfaces (3 “wet”)
Length (over everything): 16,80m

Span: 14,25m (max.)

Height: 4,37m

Engagements weight when starting: 20.1 tons (max.)

Machine: zwo Turmanski R-33D
Spitzengeschw.: Mach 2.35 with afterburner Maximum range: 1705 km
Transfer
Fuel capacity: 5000 l (internal)/1500 l (external)
Ceiling: 17500m
Maximum pay load: 3 tons

Variants: MIG-29 UB of zwositziger coaches
MIG-29K
carrier supported In use: ehem. Warsaw Pact, Yugoslavia, Poland. Germany and others Manufacturer: Mikojan Gurewitsch /1983
status: Production runs

Tuesday, April 10, 2007

MiG 15 Mikoyan 15 UTI





Specifications

Aircraft Type: MIKOYAN (Soviet Union) MiG-15 2 Seater Fighter Trainer
Performance: Maximum Speed 652 mph (1,050km/h) at sea level.
Initial Climb: 8,268 ft/min (42m/sec)
Power Plant: One Klimmov RD-45F (Rolls Royce Nene derivative) centrifugal turbojet rated at 2,270kg static thrust.
Fuel: Internal fuel capcity 1,460 litres. Optional drop tanks capacity 1,920 litres.
Weights: Empty equipped: 3382kg. Normally loaded (clean): 4806kg.
Armament: One 39mm Nudelman N-37 cannon with 40 rounds and two 23mm Nudelman-Sureanov NS-23KN cannon with 80 rpg