Bomber of airplane

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B-2 spirit

F117-A

B1-lancer

Northrop Grumman B-2A Spirit

B-2
Name: B-2 Spirit
Length: 21m03
height: 5m18
Ceiling: 16765 m
Span: 52m43
Engines: 4
Crew:
2 / 3
Max Speed: 1103 km/h
Weight Max: 181437 kg
1997 - USA Range:
13898 km

Features
Along with the B-52 and the 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 B-2 has a crew of two pilots, an aircraft commander 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.

Lockheed F-117A Nighthawk

Developing Nation: United States, by Lockheed.
First Flight(s): January / February 1978
Wing Span: 13,20 M1
Height: 3,78 M1
Length: 20,08 M1
Weight empty: 13.608 Kg.
Weight Max. Load: 23.184 Kg.
Engines: two General Electric F404-GE-F1D2
Max. Speed: 933 Kph.
Max. Range:

Combat Range 1448 Km.

Weapons:From two internal Bays, with extending pylons.

BLU-109 deep-penetration bombs

GBU-10 Paveway II

GBU-27 Paveway III

Laser-guided Mk84 bombs

Mk61 nuclear

USAF, F-117A Nighthawk, 83-0807/HO, 415th FS, Gilze Rijen AFB (The Netherlands) Photo R.Vogelaar.

The F-117A is a single-seat, wedge-shaped, V-tailed low observable night attack fighter with the technology to reduce its vulnerability to radar detection (stealth). The F-117A is not intended for air-to-air combat, its purpose to deliver ordnance (precision-guided bombs) in a dense threat environment against targets of extremely high value. During 1975, Lockheed's Skunk Work engineers began working on an aircraft which would have a greatly reduced radar cross section that would make it all but invisible to enemy radars.

 

Rockwell B-1 Lancer

The variable geometry B-1 bomber was designed as the successor for the elderly B-52. The B-1A was cancelled, partly because the high- flying bomber was obsolete, and partly for political reasons. The B-1B Lancer version, more optimized for low-altitude attacks and stealth, is now built in small numbers.

 

Type: B-1B
Function: bomber
Year: 1986
Crew: 4
E
Speed: 1375 km/h
Ceiling: 14600 m
Range: 12000 km

Armament: 29030 kgs
Unit cost: 200 million USDngines:
4 * 13600 kg G.E. F101-GE-11
Wing Span: 41.67 m/23.84 m
Length: 44.81 m
Height: 10.36 m
Wing Area: 181.16 m2
Max.Weight: 216364 kg