Aircrafts

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[Ανεβάζετε τα θέματα των εξετάσεων στον τομέα Downloads]

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[ονόματα των αρχείων]

Ανεβάζετε τα θέματα των εξετάσεων στον τομέα Downloads

με προσοχή στα ονόματα των αρχείων!

[aliakmwn]

Χωρίς τα "φονικά αυτά" όπλα , οι Τούρκοι θα φτάνανε μέχρι την Σαλονίκη κάθε μέρα. Δεύτερον, μου θυμίζεις παιδί των λουλουδιών της δεκαετίας του 60 που ονειρεύεται έναν όμορφο κόσμο χωρίς πολέμους. Λες εμένα να με αρέσουν οι πόλεμοι? Αλλά μετά την 11η Σεπ. όλα είναι φλου και ζούμε με μια αβεβαιότητα, η οποία θα μεγάλωνε αν δεν υπήρχαν αυτές οι ΑΜΥΝΤΙΚΕΣ μηχανές.

Οσες 11 Σεπτεμβρη κι αν συμβουν, οσα αεροπλανα κι αν αγοραστουν, η ειρηνη δεν θα ειναι ποτε εξασφαλισμενη οσο κουμαντο στον πλανητη κανουν οι κεφαλαιοκρατες.

Τα παιχνιδακια μεταξυ ελληνων και τουρκων γινονται γιατι ο αμερικανος εμπορος πολεμικων αεροσκαφων θελει να πλουτιζει. Οσο κυβερνουν τα τσιρακια του, αυτος θα πλουτιζει, και οι λαοι θα σκοτωνονται.

Ποια ειναι η λυση λοιπον?

Οι λαοι να στρεψουν ενωμενοι τα ντουφεκια τους εναντιον των μεγαλεμπορων πολεμικων μηχανων και των μαριονετων τους...

<<...μου θυμίζεις παιδί των λουλουδιών της δεκαετίας του 60 που ονειρεύεται έναν όμορφο κόσμο χωρίς πολέμους...>>

Πρωτα μας στερησαν τον κοσμο που ονειρευομαστε.
Και τωρα προσπαθουν να μας στερησουν και τα ιδια μας τα ονειρα...

Ας ειναι ομως, θα 'ρθει η ωρα...........................

[Megawatt]

Ποια ειναι η λυση λοιπον?

Οι λαοι να στρεψουν ενωμενοι τα ντουφεκια τους εναντιον των μεγαλεμπορων πολεμικων μηχανων και των μαριονετων τους...

Πολύ σωστά τα λες aliakmwn, αλλά πρακτικά αυτό για να γίνει και όταν γίνει εσύ και εγώ θα έχουμε πεθάνει...

[Verminoz]

Ή όταν όλος ο κόσμος θα έχει πεθάνει

[aliakmwn]

Πολύ σωστά τα λες aliakmwn, αλλά πρακτικά αυτό για να γίνει και όταν γίνει εσύ και εγώ θα έχουμε πεθάνει...

Ξεκινα λοιπον κι εσυ να προσπαθεις και να αγωνιζεσαι, για να μην ερθει σε 60 χρονια το εγγονι σου, στο μελλοντικο forum, και να λεει "Πολυ σωστα τα λες aliakmwn Γ', αλλα πρακτικα αυτο για να γινει και οταν γινει εσυ και εγω θα εχουμε πεθανει..."

[Megawatt]

Aliakmwn, εδώ τόσα χρόνια δεν δόθηκε λύση στο Κυπριακό ή στο Μεσανατολικό ή ακόμα και στο Ελληνοτουρκικό (με τον ορισμό της υφαλοκρυπίδας)-προβλήματα που αφορούν κάποιες μόνο χώρες, θα δοθεί λύση στο να σταματήσει η ξέφρενη επεκτατική πολιτική των Αμερικάνων που θέλουν να κατακτήσουν όλο τον κόσμο? ΄Δεν λέω να σταματήσουμε κάθε αγώνα, αλλά ας είμαστε και λίγο ρεαλιστές και μην αιθεροβατούμε.
===============================================

C-130 Hercules

C-130 Hercules Specifications

Primary Function: Tactical and intratheater airlift
Contractor: Lockheed
Crew: Five (two pilots, a navigator, flight engineer and loadmaster)
Unit Cost: C-130J, $48.5 million (FY98 constant dollars)

Powerplant
  Four Allison T56-A-15 turboprops; 4,300 horsepower, each engine

Dimensions
Length: 97 feet, 9 inches (29.3 meters)
Wingspan: 132 feet, 7 inches (39.7 meters)
Height: 38 feet, 3 inches (11.4 meters)

Weights
Empty: 69,300 lb (31434 kg) -- equipped C-130F
Maximum Takeoff: 155,000 pounds (69,750 kilograms)

Performance
Speed: 374 mph (Mach 0.57) at 20,000 feet (6,060 meters)
Ceiling: 33,000 feet (10,000 meters) with 100,000 pounds (45,000 kilograms) payload
Range: N/A

Armament
  N/A

C-130 Hercules Achievements

The C-130 Hercules is the West's most widely used and versatile military transport.
 

C-130 Hercules Features

  Using its aft loading ramp and door the C-130 can accommodate a wide variety of oversized cargo, including everything from utility helicopters and six wheeled armored vehicles to standard palletized cargo and military personnel. In an aerial delivery role, it can air drop loads up to 42,000 pounds or use its high-floatation landing gear to land and deliver cargo on rough, dirt strips.

  The flexible design of the Hercules enables it to be configured for many different missions, allowing for one aircraft to perform the role of many. Much of the special mission equipment added to the Hercules is removable allowing the aircraft to revert back to its cargo delivery role if desired. Additionally, the C-130 can be rapidly reconfigured for the various types of cargo such as palletized equipment, floor loaded material, air drop platforms, container delivery system bundles, vehicles and personnel or aeromedical evacuation.

  The C-130J is the latest addition to the C-130 fleet and will replace aging C-130E's. The C-130J incorporates state-of-the-art technology to reduce manpower requirements, lower operating and support costs, and provide life cycle cost savings over earlier C-130 models. Compared to older C-130s, the J model climbs faster and higher, flies farther at a higher cruise speed, and takes off and lands in a shorter distance. The C-130J-30 is a stretch version, adding 15 feet to fuselage, increasing usable space in the cargo compartment.

  C-130J/J-30 major system improvements include: advanced two-pilot flight station with fully integrated digital avionics; color multifunctional liquid crystal displays and head-up displays; state-of-the-art navigation systems with dual inertial navigation system and global positioning system; fully integrated defensive systems; low-power color radar; digital moving map display; new turboprop engines with six bladed, all composite propellers; digital auto pilot; improved fuel, environmental and ice protection systems; and an enhanced cargo handling system.

C-130 Hercules Background

  Four decades have elapsed since the Air Force issued its original design specification, yet the remarkable C-130 remains in production. The initial production model was the C-130A, with four Allison T56-A-11 or -9 turboprops. A total of 219 were ordered and deliveries began in December 1956. The C-130B introduced Allison T56-A-7 turboprops and the first of 134 entered Air Force service in May 1959.

  Introduced in August of 1962, the 389 C-130E's that were ordered used the same Allison T56-A-7 engine, but added two 1,290 gallon external fuel tanks and an increased maximum takeoff weight capability. June 1974 introduced the first of 308 C-130H's with the more powerful Allison T56-A-15 turboprop engine. Nearly identical to the C-130E externally, the new engine brought major performance improvements to the aircraft.

  The latest C-130 to be produced, the C-130J entered the inventory in February 1999. With the noticeable difference of a six bladed composite propeller coupled to a Rolls-Royce AE2100D3 turboprop engine, the C-130J brings substantial performance improvements over all previous models, and has allowed the introduction of the C-130J-30, a stretch version with a 15-foot fuselage extension. Air Force has selected the C-130J-30 to replace retiring C-130E's. Approximately 168 C-130J/J-30s are planned for the inventory. To date, the Air Force has purchased 29 C-130J aircraft from Lockheed Martin Aeronautics Company.
 

C-130 Hercules Photos

[Megawatt]

CH-47 Chinook

CH-47 Chinook Specifications

Primary Function: Medium-lift helicopter
Contractor: Boeing
Crew: Cockpit-crew seats: 2
Cabin-troop seats/litters: 33/24
Unit Cost: N/A

Powerplant
  Two Textron Lycoming T55-L-712 turboshafts each rated at 3,750 shp for takeoff and 3,000 shp for coninuous running

Dimensions
Length: 98ft 10.75 in
Rotor Diameter: 60 feet (18.29 m) each -- CH-47D
Height: 18 ft 11 in

Weights
Empty: 22,379 lb
Maximum Takeoff: 50,000 lb

Performance
Speed: 159 mph (cruising)
Ceiling: 22,100 ft
Range: N/A
 
Armament
  N/A

CH-47 Chinook Achievements

During Desert Storm the CH-47D often provided the only means of transportation to shift large numbers of personnel, equipment, and supplies quickly.

CH-47 Chinook Photos

[jimi]

Όπως και να έχει αυτά τα αεροπλάνα παρουσιάζουν τεχνικό ενδιαφέρον...Αφήστε τα περί ειρήνης κατά μέρος...Αν βλέπατε εκείνο το ντοκυμαντέρ στην ΕΤ1 για το βομβαρδιστικό Β-2 και τις συνεντευξεις κάποιων πιλότων θα είχατε φρικάρει τόσο πολύ που αυτό το topic θα σας φαινόταν μια χαρά....

Άντε να μη κάνω ένα topic με κιθάρες....

[Megawatt]

B-2 Spirit

B-2 Spirit Specifications

Primary Function: Multi-role heavy bomber
Contractor: Northrop Grumman Corp.
Crew: Two pilots
Unit Cost: Approximately $1.157 billion

Powerplant
  Four General Electric F-118-GE-100 engines (17,300 lb each)

Dimensions
Length: 69 feet (20.9 meters)
Wingspan: 172 feet (52.12 meters)
Height: 17 feet (5.1 meters)

Weights
Empty: 162,000 lb (73,482 kg)
Typical Takeoff: 336,500 lb (152,634 kg)

Performance
Speed: High subsonic
Ceiling: 50,000 feet (15,152 meters)
Range: Intercontinental, unrefueled

Armament
     NUCLEAR    CONVENTIONAL              PRECISION
     16 B61                  80 MK82                   16 JDAM (2,000 lb GBU-31)
     16 B83                  16 MK84                    8 AGM-154 JSOW
                                36 CBU87                   8 GBU-37 Bunker Busters
                                36 CBU89                8 EGBU-28 (Enhanced GBU-37)
                                36 CBU97                   AGM-158 (JASSM)

Service Life
First Flight: July 17, 1989 (B-2)
End of Service: N/A
Number Built: [21 total]

B-2 Spirit Achievements

In support of Operation Enduring Freedom, the B-2 flew one of its longest missions to date from Whiteman to Afghanistan and back.

B-2 Spirit Photos

[Megawatt]

B-2 Spirit Features

  Along with the B-52 and B-1B, the B-2 provides the penetrating flexibility and effectiveness inherent in manned bombers. Its low-observable, or "stealth," characteristics give it the unique ability to penetrate an enemy's most sophisticated defenses and threaten its most valued, and heavily defended, targets. Its capability to penetrate air defenses and threaten effective retaliation provide a strong, effective deterrent and combat force well into the 21st century.

  The revolutionary blending of low-observable technologies with high aerodynamic efficiency and large payload gives the B-2 important advantages over existing bombers. Its low-observability provides it greater freedom of action at high altitudes, thus increasing its range and a better field of view for the aircraft's sensors. Its unrefueled range is approximately 6,000 nautical miles (9,600 kilometers).

  The B-2's low observability is derived from a combination of reduced infrared, acoustic, electromagnetic, visual and radar signatures. These signatures make it difficult for the sophisticated defensive systems to detect, track and engage the B-2. Many aspects of the low-observability process remain classified; however, the B-2's composite materials, special coatings and flying-wing design all contribute to its "stealthiness."

  The B-2 has a crew of two pilots, a pilot in the left seat and mission commander in the right, compared to the B-1B's crew of four and the B-52's crew of five.

[Megawatt]

B-2 Spirit Background

 The first B-2 was publicly displayed on Nov. 22, 1988, when it was rolled out of its hangar at Air Force Plant 42, Palmdale, Calif. Its first flight was July 17, 1989. The B-2 Combined Test Force, Air Force Flight Test Center, Edwards Air Force Base, Calif., is responsible for flight testing the engineering, manufacturing and development aircraft as they are produced. .

  Whiteman AFB, Mo., is the B-2's only operational base. The first aircraft, Spirit of Missouri, was delivered Dec. 17, 1993. Depot maintenance responsibility for the B-2 is performed by Air Force contractor support and is managed at the Oklahoma City Air Logistics Center at Tinker AFB, Okla..

  The success of the B-2 was proved in Operation Allied Force, where it was responsible for destroying 33 percent of all Serbian targets in the first eight weeks, by flying nonstop to Kosovo from its home base in Missouri and back. In support of Operation Enduring Freedom, the B-2 flew one of its longest missions to date from Whiteman to Afghanistan and back..

  The prime contractor, responsible for overall system design and integration, is Northrop Grumman Integrated Systems Sector. Boeing Military Airplanes Co., Hughes Radar Systems Group, General Electric Aircraft Engine Group and Vought Aircraft Industries, Inc., are key members of the aircraft contractor team. Another major contractor, responsible for aircrew training devices (weapon system trainer and mission trainer) is Hughes Training Inc. (HTI) - Link Division, formerly known as CAE - Link Flight Simulation Corp. Northrop Grumman and its major subcontractor HTI, are responsible for developing and integrating all aircrew and maintenance training programs.

[Megawatt]

Όπως και να έχει αυτά τα αεροπλάνα παρουσιάζουν τεχνικό ενδιαφέρον...Αφήστε τα περί ειρήνης κατά μέρος...Αν βλέπατε εκείνο το ντοκυμαντέρ στην ΕΤ1 για το βομβαρδιστικό Β-2 και τις συνεντευξεις κάποιων πιλότων θα είχατε φρικάρει τόσο πολύ που αυτό το topic θα σας φαινόταν μια χαρά....

jimi δεν το είδα το ντοκυμαντέρ αλλά φαντάζομαι 
==============================================

S-37 Berkut

S-37 Berkut Specifications

Primary Function: N/A
Contractor: Sukhoi
Crew: One
Unit Cost: N/A

Powerplant
  two Aviadvigatel D-30F6 afterburning turbofans at 68,340 lb (303.8 kN) each (original)

two Saturn/ Lyul'ka AL-37FU afterburning turbofans at 63,930 lb (284.4 kN) each w/ afterburner (planned)
 
Dimensions
Length: 72.83 ft (22.60 m)
Wingspan: 74.00 ft (16.70 m)
Height: 19.33 ft (5.90 m)

Weights
Empty: N/A
Maximum Takeoff: 74,955 lb (34,000 kg)
 
Performance
Speed: 1,555 mph (2,500 km/h)
Ceiling: 61,680 ft (18,800 m)
Range: 2,100 nm (3,880 km) -- typical

Armament
  N/A

S-37 Berkut Achievements

The S-37 was built to validate and gain experience with various advances in technology that could be incoorperated in a future Sukhoi fighter.
 

S-37 Berkut Photos

[Megawatt]

Dassault Mirage 2000

Dassault Mirage 2000 Specifications

Primary Function: Interceptor [Mirage 2000C]; All weather night and day missions [Mirage 2000D]
Contractor: Dassault
Crew: One, trainer--two
Unit Cost: N/A

Powerplant
  SNECMA M 53 P2 jet engine / 9.7 t with afterburner

Dimensions
Length: 50 ft, 3 in (14.36 m)
Wingspan: 29 ft, 5 in (9.13 m)
Height: 17 ft, 0.75 in (5.20 m) -- Mirage 2000C
 
Weights
Empty: 7,600 kg -- Mirage 2000C
Maximum Takeoff: 37,478 lb (17,000 kg) -- Mirage 2000C

Performance
Speed: Maximum level speed 'clean' at 36,090 ft (11000 m) more than 1,453 mph (1,262 kt / 2338 km/h) -- Mirage 2000C
Ceiling: Above 50,000 ft / 16,500 m
Range: Combat range over 920 miles (800nm / 1480 km) -- Mirage 2000C
 
Armament
  2 AM.39 Exocet, 1 1300 L drop Tank (855 nm)
1 1300 L drop tank, 2 ARMAT, 2 R.550 Magic (885 nm)
1 1300 L drop tank, 2R.500 Magic, 2 R.530D (885 nm)
4 Belouga, 2 1700 L drop tank, 2 R.550 Magic (1094 nm)
18 EU2 250 kg bombs (756 nm)

Dassault Mirage 2000 Achievements

No known major achievements

Dassault Mirage 2000 Photos

[Megawatt]

A-7 Corsair II

A-7 Corsair II Specifications

Primary Function: Attack
Contractor: Ling-Temco-Vought (Prime, now Northrop Grumman Corp.)
Crew: One
Unit Cost: $2,860,000 (A-7D)

Powerplant
  Single Allison/Rolls Royce TF41-A-400 non-afterburning turbofan engine with a static thrust rating of 15,000 pounds

Dimensions
Length: 46 feet 1.5 inches
Wingspan: 38 feet 9 inches
Height: 16 feet 1 inch

Weights
Empty: 19,111 lb (8668 kg)
Maximum Takeoff: 42,000 lb (19050 kg)

Performance
Speed: 595 knots (685 mph / 1102 km/h)
Ceiling: 45,000 ft
Range: 3,224 miles

Armament
  One internally mounted M61A1 20 mm six barrel cannon
Six wing pylons
Two fuselage launch stations
Pylons can carry a large single weapon, multiple racks capable of six weapons per rack, or triple racks with three weapons per rack.
Can carry 15,000 pounds of payload
Compatible with practically all first line ordnance used by the U.S./USAF/NATO.
 
Service Life
First Flight: September 27, 1965 (A-7A)
End of Service: 1993 (still in service with Greece and Portugal)
Number Built: A-7A (199) + A-7B (196) + A-7C (67) + 1,107 others [~1,569 total]

A-7 Corsair II Achievements

One of the most accurate strike aircraft ever built

A-7 Corsair II Features

  The A-7 Corsair II was built on the F-8 Crusader airframe, and was a subsonic attack version of this fighter. It was exceptionally accurate, and was purchased by the US Navy and Marines, and later on by the US Air Force. The A-7 was first flown on September 27, l965, and initial deliveries began on October 14, l966. With a typical weapons load, the A-7E would have a tactical radius of 700 miles. It carried one 20-mm M61A1 multi-barrel cannon and up to 15,000 lb. of mixed stores externally.

A-7 Corsair II Background

  The A-7 Corsair II was one of a few US Navy aircraft to be operated by the US Air Force. It was created in response to the US Navy's 1963 light attack aircraft specification, which required light attack aircraft to replace the A-4 Skyhawk and with about twice the payload. 35 production A-7A's were ordered on March 19, 1964, powered by a non afterburning 12,200lb Pratt & Whitney TF-30-P-8 turbofan engine. It first flight occurred on September 27, 1965, and in 1966, the USAF ordered the A-7D (airforce version) with the Allison TF41 turbofan engine. The US Navy later developed the A-7E with TF41 engines also. The A-7 was used widely during the Vietnam War and the US Navy used them during the Gulf War as well. The A-7 was later replaced by the F/A-18 Hornet.

A-7 Corsair II Photos

[Megawatt]

Yak-141 Freestyle

Yak-141 Freestyle Specifications

Primary Function: Carrier Based Interceptor
Contractor: Yakovlev
Crew: One
Unit Cost: N/A

Powerplant
  One Kobchenko/Soyuz R-79-300 turbofan engine rated at 34,170lb for takeoff, two Rybinsk RD- 41 turbofan engines rated at 9,039lb for lift

Dimensions
Length: 60 ft 2 in
Wingspan: 33 ft 1.5 in (spread)
19 ft 4 in (folded)
Height: 16 ft 4 in

Weights
Empty: 25,684 lb
Maximum Takeoff: 34,833 lb vertical, 42,990 lb short

Performance
Speed: 1148.4 mph (Mach 1.8 )
Ceiling: 49,000 ft
Range: 1306.8 mi

Armament
  One 30mm cannon, Alamo and Archer AAMs, bombs, and rockets

Yak-141 Freestyle Achievements

The Yak-141 is the world's first supersonic STOVL aircraft
 

Yak-141 Freestyle Photos

[Megawatt]

Dassault Rafale

Dassault Rafale Specifications

Primary Function: Multi-role fighter / reconn.
Contractor: Dassault 
Crew: Single or twin seater 
Unit Cost: N/A

Powerplant
  Two SNECMA M88-3 turbofans each rated at 19,555 lb (86.98 kN) with afterburning -- Rafale C

Dimensions
Length: 50 ft 3 in (15.3 m)
Wingspan: 35 ft 9 in (10.9 m)
Height: 17 ft 6 in (5.34 m)

Weights
Empty: N/A
Maximum Takeoff: 47,399 lb (21500 kg) -- Rafale C

Performance
Speed: Maximum level speed 'clean' at 36,090 ft (11000 m) 1,321 mph (1,147 kt / 2125 km/h) -- Rafale C
Ceiling: 60,000 ft
Range: 1000 nm

Armament
  Cannon: 1 30mm DEFA 554; Mica, R.550 Magic 2, BGL 400

Dassault Rafale Achievements

No known major achievements

Dassault Rafale Photos