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[Αντιστοίχηση Μαθημάτων ΝΠΣ με ΠΠΣ]

Επίσημη ενημέρωση για Αντιστοίχηση Μαθημάτων ΝΠΣ με ΠΠΣ και η συζήτηση στο forum.

[Megawatt]

TU-95/MS Bear

τι σε έκανε να ποστάρεις αυτό το αεροπλάνο?

Το TU-95 είναι η "ρωσική απάντηση" στο αμερικανικό βομβαρδιστικό Β-52. Τώρα μή με ρωτήσεις τί με έκανε να ποστάρω το Β-52!      

Τιποτα σε Αirbus 320 παίζει?
Δεν ξέρω για εσάς, αλλά εγω αισθάνομαι πιό ασφαλης οταν ταξιδεύω με αυτά παρά με τα Βoeing 737.  Το λέει και το όνομα άλλωστε, όταν πέφτουν κανουν μπόινγκ! (βλακ χιούμορ)

Αφιερωμένο:

χθες εβλεπα στο discovery channel ενα ντοκιμαντερ για πολεμικα αεροσκαφη κ το πιο εξελιγμενο της τεχνολογιας στελθ ειναι ενα Raptor 22.τεταρτης γενιας ελεγαν.το δικιμαζαν 20 χρονια!!αν το βρω πουθενα θα το στειλω.

Μια πιο προσεκτική ματιά στο τόπικ αυτό:
F-22 Raptor
X-35 JSF 
==================================================

Airbus A320

Airbus A320 Specifications

Primary Function: Commercial Transport
Contractor: Airbus
Crew: 164 single class, 150 double class
Unit Cost: N/Α

Powerplant
  Two CFM56-5 or IAE V2500 engines rated at 25,000-27,000 lb thrust

Dimensions
Length: 123 feet, 3 in
Wingspan: 111 feet, 10 in
Height: 39 feet, 7 in

Weights
Empty: 92,400 lb
Maximum Takeoff: 169,800 lb

Performance
Speed: Mach 0.82
Ceiling: N/A
Range: 3,050 nm

Armament
  N/A

Airbus A320 Achievements

No known major achievements

Airbus A320 photos

[Megawatt]

F-16XL

F-16XL Specifications

Primary Function: experimental - Laminar Flow Research Aircraft
Contractor: General Dynamics Corp.
Crew: One
Unit Cost: N/A

Powerplant
  Pratt and Whitney 100-PW-100 engine (with afterburner), rated at 23,830 lb thrust

Dimensions
Length: 54.2 ft (16.52 m)
Wingspan: 34.3 ft (10.45 m)
Height: 17.7 ft (5.39 m)

Weights
Empty: N/A
Max. Weight: 48,000 lb (17,915.60 kg)

Performance
Speed: Mach 1.8 (1,260 mph)
Ceiling: 50,000 ft
Range: 2,850 miles

Armament
  N/A

F-16XL (Ship #2) Specifications

Primary Function: experimental - Laminar Flow Research Aircraft
Contractor: General Dynamics Corp.
Crew: Two
Unit Cost: N/A

Powerplant
  General Electric F110-GE-129 engine (with afterburner) rated at 29,000 lb thrust

Dimensions
Length: 54.2 ft (16.52 m)
Wingspan: 34.3 ft (10.45 m)
Height: 17.7 ft (5.39 m)

Weights
Empty: N/A
Max. Weight: 48,000 lb (17,915.60 kg)
 
Performance
Speed: Mach 2 (1,400 mph)
Ceiling: 50,000 ft
Range: 2,850 miles
 
Armament
  N/A

F-16XL Achievements

The F-16XL was the first program to look at laminar flow on swept wings at speeds representative of those at which a high speed civil transport might fly.
 

F-16XL Photos

[Megawatt]

F-16 AFTI

F-16 AFTI Specifications

F-16 AFTI based on F-16A (Serial #75-0750) -- F-16A stats shown
Primary Function: experimental - Advanced Fighter Technology Integration
Contractor: Lockheed (General Dynamics)
Crew: One
Unit Cost: N/A

Powerplant
  One Pratt & Whitney F100-PW-200 rated at 23,830 lb. thrust with afterburner

Dimensions
Length: 49 ft, 6 in
Wingspan: 32 ft, 10 in
Height: 16 ft, 6 in

Weights
Empty: N/A
Loaded: 29,896 lb

Performance
Speed: 1,345 mph
Ceiling: 55,000 ft
Range: 1,407 miles

Armament
  N/A

F-16 AFTI Achievements

Numerous flight avionics technologies advancements (Automatic Ground Collision Avoidance System, Real Time Kill Recognition, close air support and battlefield air interdiction, voice control system, etc.)

F-16 AFTI Photos

[Megawatt]

Su-39 Frogfoot

Su-39 Frogfoot Specifications

Primary Function: Close support/ground attack
Su-39 is an all-weather attack system capable of executinga large number of combat
missions assigned both to effectively and reliably safeguard the ground,sea and air frontiers
of the country and use the aviation of peacekeeping forces in local conflicts

Powerplant
 2 TRD-R-195, 2 x 4'300 kgs

Dimensions (m):
14,36 x 15,53 x 5,20

Weights (tonns):
16,5- 20,5

Performance:
Speed 950
Alt. (m): 18'000
Range (km): 400/500/2250

Armament:
16 AT Vihr
Kh-29T/L/ML, S-25L, Kh-58, Kh-31P, Kh-35
RVV-AE, R-73, R-60M

8 S-8/S-13 30 mm DP GSh-301
2-4 SPPU-87 (Gsh-301) bombs KAB500/1500 incl. nucl.
8 KMGU

Competitors:
A-10A Thunderbolt II

The Su-39 is intended for precise destructionof any targets on ground, sea and in the air located up to 900 km fromhome aerodromes day and night, in VFR and IFR of the weather conditionsand enemy air defense counteractions.
The aircraft features the following characteristicsthat ensure its highly effective combat use:
1. Sight/navigation system comprising:
- armament control system that provides forthe use of aboard weapons in a horizontal flight, diving, recovery fromdiving and pitching-up and two different weapon types in one attack:
- Shkval day/night automatic sight systemconstituting an optical radar with 23 power magnification of a target andterrain, including a system used for the search, identification, trackingand target designation for Vikhr missiles and weapons with laser guidancesystem, featuring 0.6 m guidance precision;
- Kopiye-25 radar sight system operatingin a 3 cm band of electromagnetic waves intended for detection and targetdesignation in "air-to-surface", "air-to-air", "air-to-sea"modes of operation and in a cartography mode;
- navigation aids providing for automatictarget approach with up to 15 meter precision irrespective of a flightrange.
2. The electronic countermeasure (ECM)system is intended to carry out electronic reconnaissance and all-directionalprotection of aircraft in radar and IR band of electromagnetic waves inautomatic mode of operation without the pilot’s interference.
The system comprises:
- electronic reconnaissance set intendedto pinpoint all existing ground, airborne and shipborne radars used fordetection and fire-control, operating in 1.2-18 GHz and determine the mostdangerous target, its coordinates and distance to it;
- small-size electronic active jammer, generatingdeflecting, noise, scintillating and re-targeting to underlying surfaceinterferences;
- optronic jammer, generating an amplitude-frequencymodulating interference to IR missile seekers;
- dispenser of IR decoys with 192 decoy projectilesgenerating passive jamming in conjunction with "cold" aircraftengines intended to frustrate at a critical moment over a target the ADmissile portable systems of enemy attack;
- aircraft decoys to detect and deceive ADenemy systems lurking in ambushes, onboard fighter radars and missileswith all types of seekers.
3. The large nomenclature of precession weapons,including "air-to-surface", "air-to-sea", "air-to-air"and "air-to-radar" missiles and all nomenclature of cheap andeffective means of destruction: 85-250mm rockets, 30mm guns and air bombsup to 500 kg weighing up to 6,000 kg.
However, the Vikhr antitank missile is themain versatile weapon of the Su-39. The aircraft is armed with 16 suchmissiles capable of directly hitting a moving tank at a 10 km range featuringup to one meter of reduced armoring, rapid boats, rapid maneuvering helicoptersand heavy aircraft.
4. The unique effectiveness of a combat survivalsystem, providing for a 100 % protection of the pilot and vital parts ofan aircraft from 30mm gun rounds and missile splinters and returning theaircraft to its home aerodrome when hit by an AD portable Stinger typemissile system.
The high efficiency of the Vikhr system wasrevealed during combat employment of the Su-25 in armed conflicts worldwide.The total weight of combat survival equipment of the Su-39 is equal to1,115 kg.
5. The high aircraft maneuverability enablesit at low and average altitudes and speeds to rotate "on its tail"and launch a second attack almost without visual loss of contact with anair and ground (surface) target, especially in limited space over the target- in hard accessible forest and mountainous areas, when the use of otherstrike systems is virtually impossible.
6. The high reliability of the Su-39 andits systems was revealed by extended operation of the Su-25 attack aircraft.
7. The Su-39 capability to perform take-offand landing with a combat payload on poorly prepared earth runways, includingthose located in the mountains up to 3,000 m high at sea level and up to1,200 meters long, thereby making the Su-39 appropriate for combat usein close vicinity to combat actions region ensuring a rapid change of aircraftbasing and the rapid delivery surprise blows on the enemy.
8. The technical-economical indices characterizethe Su-39 in any kind of operation as the "genuine soldier" weapon.
The Su-39 is:
- cheapest and effective attack aircraftof its type;
- most undemanding - can use diesel fuelinstead of kerosene and does not require high-skilled maintenance. Pilotsof any grade can muster the aircraft;
- the aircraft boasts a 30 year service life,involving routine repairs of an air frame and engine at home aerodromes.
The various and highly effective armamentof the Su-39 used in conjunction with an on-board armament control system,sight/navigation system, ECM devices and combat survivability, constitutea powerful attack system capable of executing a large number of combatmissions assigned to effectively and reliably safeguard the ground, seaand air frontiers of the country. The aircraft was put in series productionin 1995.

Su-39 Frogfoot Photos

[Megawatt]

IL-102

IL-102 Specifications

Primary Function: Ground attack
Contractor: Ilyushin
Man./Crew: 1

Powerplant
4 D30kp, 11'984 kgs

Dimensions (m)
50,0 x 47,0 x 15,0

Weights (tons)
72,0-157

Performance
Speed (km/h): 900
Alt. (m): 14'000
Range (km): 5'000

Armament:
AA
AS 23 mm DP NR-23 ,bombs KAB500/1500 incl. nucl. 13 tons

Competitors:
A-10A Thunderbolt II

Il-102 has made the first flight in 1982. The new plane has passed state tests, however solution about batch production was not accepted. In a series was started attack jet by Sukhoi OKB Su-25. In 1992 Il-102 was on display on the Russian airspace exhibition “Mosaeroshow-92” and was offered on sale for the representatives of foreign countries. Il-102 is further development first Soviet attack plane with TRD IL-40, created in 1953. Il-102 is made under the normal aerodynamic scheme with low-set wing. The features of arrangement of a plane Il-40 are saved: crew consisting of the 2 persons, fuel tanks and two drives are placed in a central part near to centre of masses of a plane, that has allowed to reduce square of booking and to improve manoeuvrable qualities of attack jet. The wing of a plane has a rather thick structure permitting to place in its rooted part 6 bomb baies. Wings directed downwards, in their face parts the place for installation of the block of an ejection “automaton - F” with IR by traps and dipole reflectors is stipulated. Kiel with a developed dorsal fin is supplied with a control surface of a direction.


The fuselage has characteristic “hump”, in which the cabins of the pilot, arrow, part BREO and fuel tanks are located. In a tail part on each side of fuselage two aerodynamic brakes are installed. A forward and back cabin have flat armourglass. Three based chassis ensures a possibility of operation of a plane with ground landing, capable to sustain pressure 5 kg/sm2. The fuel is placed in 6 protected tanks located in a central part of a fuselage and the protected reservations. On two underfuselage knots of the external suspension two can be suspended PTB till 800 litres. The power plant consists of two unafterburning DTRD (variant of drives installed on the fighter Mig-29). The application of a reversion and system of a deviation(rejection) of thrust vector is supposed. In a cabin of the pilot the collimating sight S-17BTs is installed, the possibility of application of a radiosight and optic-electronic aim systems is stipulated. Arrows is equipped with an aim system KPS-53-A, including a sight PAU-475-2M with an optical range finder and calculator. The plane is equipped with ejected seats K-36A. As a whole Il-102 on main performances is similar to American A-10A.

IL-102 Photos

[Megawatt]

SR-71 Blackbird

SR-71 Blackbird Specifications

Primary Function: Strategic Reconnaissance
Contractor: Lockheed-Martin Skunkworks
Crew: Two
Unit Cost: N/A
 
Powerplant
  Two Pratt and Whitney J-58 axial-flow turbojets with afterburners, each producing 32,500 pounds of thrust 

Dimensions
Length: 107.4 feet (32.73 m)
Wingspan: 55.6 feet (16.94 m)
Height: 18.5 feet (5.63 m)

Weights
Empty: N/A
Maximum Takeoff: 140,000 pounds (52,250 kg) -- gross

Performance
Speed: over Mach 3.2 / 2,000 mph (3,200 kph)
Ceiling: over 85,000 feet (26,000 m)
Range: over 2000 miles (3200 km) unrefueled

Armament
  N/A

SR-71 Blackbird Achievements

The SR-71 Blackbird is the fastest aircraft in the world to take off under its own power. 

SR-71 Blackbird Background

  Developed for the USAF as reconnaissance aircraft more than 30 years ago, SR-71s are still the world's fastest and highest-flying production aircraft. The aircraft can fly more than 2200 mph (Mach 3+ or more than three times the speed of sound) and at altitudes of over 85,000 feet. As research platforms, the aircraft can cruise at Mach 3 for more than one hour.

SR-71 Blackbird Photos

[Megawatt]

Canadair CL-415

Canadair CL-415 Specifications

Primary Function: waterbomber
Cost Approx. $35 million (Canada) 
Crew 2
Passengers 8 / 30 with tanks removed

Power Plant
Engines 2 x Pratt & Whitney Canada PW123AF turboprops
Power 2 x 1775 kW (2380 shp)
Propeller Hamilton Standard 14SF-19 four-blade, diameter 3.97 m
Fuel consumption 840 litres/hour typical

Dimensions
Length 19.82 m
Height 8.98 m
Span 28.61 m
Wing area 100.33 sq m
Cabin length 9.38 m excluding cockpit
Cabin width 2.39 m maximum
Cabin height 1.90 m
Cabin volume 35.6 cu m excluding cockpit

Weights
Operating weight empty 12861 kg
Max. payload 6123 kg
Integral water tank capacity 6160 litres (1622 US gal)
Fuel capacity 5796 litres (1530 US gal)
Max. zero-fuel weight 19051 kg
Max. ramp weight 19958 kg
Max. take-off weight 19890 kg on land, 17169 kg w\o disposable load
Max. lift-off weight after water scoop 20865 kg
Max. landing weight 16783 kg

Performance
Max. cruise speed  376 km/h at 5000 ft/ISA
Initial rate of climb 7 m/s at max. weight
Takeoff distance 844 m or 814 m on water
Landing distance 674 m on land, 664 m on water
Max. Range 2427 km (1310 NM)
Water dropped per hour 54140 l, when 11 km from fire
Scooping time to refill tanks 12 seconds

Armament
  N/A

Canadair CL-415  Background

The Canadair 415 is the latest in Canadair's line of multi-role amphibious aircraft beginning with the CL-215 in the 1960s. The Canadair 415 amphibian is a high-wing, turboprop aircraft that evolved from over 25 years of experience with the CL-215 firefighting amphibious aircraft. It features a four-compartment, four-door water tank system that can hold 6137 litres (1621 US gallons) of water/foam mixture and refills its tanks by skimming the surface of any suitable body of water. The Canadair 415, although externally similar to its predecessor, is quite a new machine. It features Pratt & Whitney Canada turboprops, an air-conditioned glass cockpit, and powered flight controls. Compared to the CL-215, it has increased operating weight and speed yielding improved productivity. Aircraft systems have been updated for easier maintainability. In its firefighting configuration, the Canadair 415 is ideal for Initial Attack on forest fires; getting to the fire at the earliest stages and repeatedly dropping large amounts of fire suppressing foam.The Canadair 415 amphibian is also well suited to other missions such as maritime surveillance, coastal patrol, search and rescue, utility transport and resource protection The Canadair 415 production program was launched in October of 1991. The Canadair 415 first flew in December 1993 and the first aircraft was delivered in November 1994.

Canadair CL-415  Photos

[Megawatt]

Και όμως έπεσε...

http://www.thmmy.gr/smf/index.php?topic=6604.msg103891#msg103891

[ikoufis]

Ιδού το συγκεκριμένο αεροσκάφος:

[OtiNaNAi]

ANTONOV AN-225






The An-225 Mriya (Ukrainian: Антонов Ан-225 Мрія, NATO reporting name: Cossack) is a strategic airlift transport aircraft which was built by Antonov, and is the world's largest flying airplane ever built by the most commonly accepted measure, maximum gross takeoff weight. The design, built to transport the Buran orbiter, was an enlargement of the successful An-124 Ruslan. Mriya (Мрія) means "dream" (inspiration) in Ukrainian.

With a maximum gross weight of 640 tonnes (1,411,000 lb), the An-225 is the world's heaviest and largest aircraft. The Hughes H-4 Hercules, known to most as the "Spruce Goose", had a greater wingspan and a greater overall height, but is considerably shorter, and due to its lighter building materials, also lighter. In addition, the Hercules only flew once and not very high, making the An-225 the largest aircraft in the world to take off multiple times.The An-225 is also larger than the Airbus A380 airliner, and considerably bigger than the Antonov An-124, 747-400ERF, C-5 Galaxy, the nearest equivalent heavy airlifters.

In November 2004, FAI placed the An-225 in the Guinness Book of Records for its 240 records.



The An-225 was designed for the Soviet space program as a replacement for the Myasishchev VM-T. Able to airlift the Energia rocket's boosters and the Buran space shuttle, its mission and objectives are almost identical to that of the Airbus Beluga and the United States' Shuttle Carrier Aircraft.

The An-225 is an extension of Antonov's earlier An-124. To meet the needs of its new role, fuselage barrel extensions were added fore and aft of the wings, which received root extensions.Two more Lotarev D-18 turbofan engines were added to the new wing roots, bringing the total to six, and an increased-capacity landing gear system with 32 wheels was designed. The An-124’s rear cargo door and ramp were removed to save weight, and the empennage was changed from a single vertical stabilizer to a twin tail with an oversized horizontal stabilizer. The twin tail was made necessary by the requirement to carry very large and heavy external loads, which would disturb the aerodynamics of a conventional tail. Unlike the An-124, the An-225 was not intended for tactical airlifting and is not designed for short-field operation.

The An-225 first flew on December 21, 1988. Two aircraft were ordered, but only one An-225 (tail number UR-82060[4]) is currently in service. It is commercially available for carrying ultra-heavy and oversize freight, up to 250,000 kg (550,000 lb) internally or 200,000 kg (440,000 lb) on the upper fuselage. Cargo on the upper fuselage can be 70 m long.A second An-225 was partially built during the late 1980s for use by the Soviet space program. Following the collapse of the Soviet Union in 1990 and the cancellation of the Buran space program, the lone operational An-225 was placed in storage. The six Lotarev engines were removed for use on An-124s, and the second An-225 airframe (nearing completion and awaiting engines) was also mothballed.


General characteristics
Crew: 6
Payload: 250,000 kg (550,000 lb)
Door dimensions: 440 x 640 cm (14.4 x 21.0 ft)
Length: 84 m (275.6 ft)
Wingspan: 88.40 m (290 ft 2 in)
Height: 18.1 m (59.3 ft)
Wing area: 905.0 m² (9,743.7 ft²)
Empty weight: 175,000 kg (385,800 lb)
Max takeoff weight: 640,000 kg (1,322,773 lb)
Powerplant: 6× ZMKB Progress D-18 turbofans, 229 kN (51,600 lbf) each
Takeoff run: 3,500 m (11,500 ft) with maximum payload
Performance
Maximum speed: 850 km/h (460 knots, 530 mph)
Cruise speed: 750 km/h (400 knots, 465 mph)
Range:

With maximum fuel: 14,000 km (8,700 mi)
With maximum payload: 4,000 km (2,500 mi)
Service ceiling: 10,000 m (33,000 ft)
Wing loading: 662.9 kg/m² (135.5 lb/ft²)
Thrust/weight: 0.234

[Megawatt]

ANTONOV AN-225

In November 2004, FAI placed the An-225 in the Guinness Book of Records for its 240 records.

[Wade]

Δηλαδή μπαίνει στα βιβλίο Γκίνες κι αυτός που κατέχει τα περισσότερα ρεκόρ στο βιβλίο Γκίνες;  Αυτό θα πει κάψιμο