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Charles de Gaulle (R91)
Jumat, 08 Maret 2013
Heavy Expanded Mobility Tactical Truck
Heavy Expanded Mobility Tactical Truck
The HEMTT's objective is to provide heavy transport capabilities for
supply and re-supply of combat vehicles and weapons systems for the United States Army. It is distinguished by extreme mobility compared to standard 5-ton trucks,
thanks to its large number of wheels and turbo-charged engine, combined
with all-wheel drive and very large, low-pressure tires. Though far
less publicized than the Humvee, it has been extremely important in transporting logistics behind quick-moving forces based on the M1 Abrams tank.
Denel AH-2 Rooivalk
Denel AH-2 Rooivalk
| Role | attack helicopter |
|---|---|
| Builder | Denel Aerospace Systems |
| First flight | 11 February 1990 |
| Commissioning | 1,999 |
| Date of withdrawal | Still in service |
| Unit cost | $ 40 million |
| Number built | 12 |
| Crew | |
| 1 pilot + 1 operator arms | |
| Engine | |
| Engine | Makila 1K2 turboshaft |
| Number | 2 |
| Dimensions | |
| Rotor diameter | 15.58 m |
| Length | 18.73 m |
| Height | 5.19 m |
| Masses | |
| In vacuum | 5730 kg |
| Maximum | 8750 kg |
| Performance | |
| Speed | 278 km / h |
| Ceiling | 6096 m |
| Rate of climb | 799 m / min |
| Range capability | 705 km |
Leopard 2
Leopard 2
The Leopard 2 is a main battle tank of the third post-war generation with four-member crew. Conventional design executed with rear engine, it was the concept of combined arms battle anti-tank in conjunction with the armored Marder designed. He is the principal weapon system of armored troops of the Armed Forces and foreign users States. It consists of a tank with an attached self-supporting tower with a 120-mm smoothbore gun as the main armament, a smoke grenade , and two machine guns of various types depending on the user state as secondary armament. The fire control system of the tower allows the gunner , in stance as well as from the trip with stationary or moving targets to cause the fire fight.
Boeing C-17 Globemaster III
C-17 Globemaster III
The C 17 Globemaster III strategic transport aircraft is a high-capacity, designed to provide the air forces of NATO component of a modern and efficient transport. Its design is the result of a specific ' USAF
trying to modernize its fleet and transport medium and heavy at the
same time, required operational capability of spectrum, such as tactical
transport, the aviolancio means, materials and paratroopers; the
transport of injured and emergency evacuation.
| Description | |
|---|---|
| Type | Tactical transport aircraft |
| Crew | 2 pilots 1 the loading operator |
| Designer |  McDonnell Douglas |
| Builder | Boeing |
| Date first flight | May 18, 1992 |
| Date of entry into service | 1993 with the ' U.S. Air Force |
| Primary user | U.S. Air Force |
| Other users | see here |
| Specimens | 211 (as of December 2009) |
| Unit cost | 218 million $ |
| Developed by | McDonnell Douglas YC-15 |
| Dimensions and weights | |
| Length | 53.04 m |
| Wingspan | 50.29 m |
| Height | 16.76 m |
| Wing area | 353 m² |
| Wing loading | 750 kg / m² |
| Empty weight | 120 250 kg |
| Weight load | 189 375 kg |
| Maximum takeoff weight | 263 000 kg |
| Passenger | 154 passengers or 102 paratroopers |
| Capacity | 76 655 kg |
| Fuel capacity | 134 556 L |
| Propulsion | |
| Engine | 4 turboblowers Pratt & Whitney F117-PW100 |
| Push | 118.55 kN each |
| Performance | |
| Max | 0.77 Mach (approx. 817 km / h ) |
| Autonomy | from 4445 to 7564 km |
| Tangency | about 11 000 m |
F-22 Raptor
F-22A Raptor at 2008 Andrews AFB airshow
The F-22 is a jet fighter of the 5th generation capacity stealth 5th generation. It has two engines turbofan with afterburning Pratt & Whitney F119-PW-100 capable of vectored thrust . The maximum thrust is a classified information , even if most of the sources gives the value of 156 k N for propulsor. It is estimated a maximum speed of around Mach 1.82 mode Supercruise (ie without the use of afterburners ).
| Description | |
|---|---|
| Type | air superiority fighter of V generation stealth |
| Crew | 1 pilot |
| Builder |  Lockheed Martin Boeing IDS |
| Date first flight | 27 September 1990 (YF-22) |
| Date of entry into service | December 15, 2005 (F-22A) |
| Primary user | USAF |
| Specimens | 187 |
| Unit cost | 138 million U.S. $ |
| Developed by | YF-22 Lightening II |
| Other variants | X-44 MANTA |
| Dimensions and weights | |
 | |
| Length | 18.90 m (62 ft 1 in ) |
| Wingspan | 13.56 m (44 ft 6 in) |
| Wing area | 78.04 m² (840 ft ²) |
| Wing loading | 322 kg / m² (66 lb / ft ²) |
| Empty weight | 19 700 kg (43,430 lb ) (The truth is, a given weight assigned, and varies depending on the source, between 14 and 19 tons) |
| Weight load | 29 300 kg (64,460 lb) [1] |
| Maximum takeoff weight | 38 000 kg (83,500 lb) |
| Propulsion | |
| Engine | 2 turbofan Pratt & Whitney F119-PW-100 with afterburner |
| Push | from 104 to 156 kN each |
| Performance | |
| Max | 2.25 But (2410 km / h at high altitude) [2] |
| Autonomy | 2960 km |
| Range | 759 km |
| Tangency | 19 812 m |
| Armament | |
| Cannons | 1 M61A2 Vulcan 20mm |
| Bombs | free fall: 8 GBU-39 GPS guidance: 2 JDAM 2 WCMD |
| Missiles | air-to-air: 2 AIM-9 Sidewinder 6 AIM-120 AMRAAM |
| Pylons | 4 underwing 2 holds internal |
| More | version information: F-22A 'Raptor' |
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