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: 1× Volvo RM8B afterburning turbofan, 16,200 lbf dry, 28,110 lbf afterburning (72.1 kN / 125.0 kN)
Performance
- Maximum speed: Mach 2.1, 1,386 mph at 36,100 ft (2,231 km/h at 11,000 m)
- Range: 1,240 mi (2,000 km)
- Service ceiling: 59,100 ft (18,000 m)
- Rate of climb: ft/min (m/min)
Armament
- 1x 30 mm Oerlikon KCA cannon with 150 rounds
- Six missile stations for two Skyflash, four AIM-120 AMRAAM (JA 37D), or six AIM-9 Sidewinder or four 135 mm (5.4 in) rocket pods
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)
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: 4× 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
- Maximum speed: Mach 1.25 (950 mph, 1,529 km/h)
- Combat radius: 2,993 nm (3,445 mi, 5,543 km)
- Maximum range: 6,478 nm (7,456 mi, 11,998 km)
- Service ceiling: 60,000 ft (18,000 m)
- Wing loading: 167 lb/ft² (816 kg/m²)
- Thrust/weight: 0.37
Armament
- Locations:
- 6 external hardpoints for an additional 59,000 lb (27,000 kg) of ordnance (use for weapons currently restricted by START I treaty)
- 3 internal bays for 75,000 lb (34,000 kg) of ordnance.
- Options:
- Bombs:
- 84× Mk-82AIR inflatable retarder general purpose bombs[25]
- 81× Mk-82 conical general purpose bombs[26]
- 84× Mk-62 Quickstrike[27] naval mines
- 8× Mk-65 naval mines
- 30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)[28]
- 30× CBU-103/104/105 WCMD
- 24× GBU-31 JDAM GPS guided bombs (both Mk-84 general purpose and BLU-109 penetrating bombs)
- 17x GBU-38 JDAM GPS guided bombs (Mk-82 general purpose warhead)[29]
- 24× Mk-84 general purpose bombs
- Missiles:
- 24× AGM-158 JASSM
- 12× AGM-154 JSOW
- 96x or 144× GBU-39 Small Diameter Bomb GPS guided bombs (96 if using four-packs, 144 if using six-packs) (this capability has not yet been fielded on the B-1)
- Fuel: One or more of the three internal weapons bays can be configured to carry a 10,000 gallon (38,000 L) fuel tank instead of weapons in that bay)
- Bombs:
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 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 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 F3 ZG757.
Specifications (Tornado IDS GR.4)
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: 2× Turbo-Union RB199-34R Mk 103 afterburning turbofans, 43.8 kN dry, 76.8 kN afterburning (9,850 lbf / 17,270 lbf) each
Performance
- Maximum speed: Mach 2.34, 2,417.6 km/h (1,511 mph)
- Range: 1,390 km typical combat, 3,890 km ferry with four external drop tanks (870 mi / 2,420 mi)
- Service ceiling: 15,240 m (50,000 ft)
- Rate of climb: 76.7 m/s (15,100 ft/min)
- Thrust/weight: 0.55
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)
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: 4× General Electric F118-GE-100 turbofans, 17,300 lbf (77 kN) each
Performance
- Maximum speed: 410 knots (475 mph, 764 km/h)
- Range: 6,500 mi (5,600 nm, 10,400 km)
- Service ceiling: 50,000 ft (15,000 m)
- Wing loading: 67.3 lb/ft² (329 kg/m²)
- Thrust/weight: 0.205
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)
Data from Quest for Performance[35]
General characteristics
- Crew: 1
- Length: 37 ft 6 in (11.4 m)
- Wingspan: 37 ft 1 in (11.3 m)
- Height: 14 ft 8 in (4.5 m)
- Wing area: ft² (m²)
- Empty weight: lb (kg)
- Loaded weight: 13,791 lb (6,300 kg)
- Powerplant: 1× General Electric J47 turbojet, 5,200 lbf (24 kN)
- Zero-lift drag coefficient: 0.0132
- Drag area: 3.8 ft² (0.35 m²)
- Aspect ratio: 4.78
Performance
- Maximum speed: 685 mph (595 knots, 1,100 km/h)
- Range: 1,200 mi (1,000 nm, 1,900 km)
- Service ceiling: 49,000 ft (14,900 m)
- Rate of climb: 7,250 ft/min (36.8 m/s)
- Thrust/weight: 0.38
- Lift-to-drag ratio: 15.1
- Time to altitude: 6.3 min to 30,000 ft (9,145 m)
Armament
- Guns: 6× 0.50 in (12.7 mm) machine guns