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The Dongfeng-41 or DF-41 (simplified Chinese: 东风-41; traditional Chinese: 東風-41; lit. 'East Wind-41'; NATO reporting name: CH-SS-20; [4] previously reported as CSS-10 [5]) is a fourth-generation Chinese solid-fuelled road-mobile intercontinental ballistic missile operated by the People's Liberation Army Rocket Force (formerly the Second Artillery Corps).
The Taian HTF5980 is a 16x16 TEL that specialises in carrying superheavy ICBMs like the aforementioned DF-41s or sometimes the DF-31AG. [1] It is the first eight-axis self-propelled chassis made in China, equipped with a multi-axis steering system to meet the requirements of high manoeuvrability for a ground vehicle of such size.
DF-26 as seen after the 2015 Beijing military parade. The DF-26C is an IRBM with a range of at least 5,000 km (3,100 mi), far enough to reach U.S. naval bases in Guam. Few details are known, but it is believed to be solid-fuelled and road-mobile, allowing it to be stored in underground bunkers and fired at short notice, hence difficult to counter.
Specifications or photos of the X-41 program have not been released to the public; thus little is known about its goals. It has been described as an experimental maneuvering reentry vehicle capable of transporting a 1,000-pound payload on a sub-orbital trajectory at hypersonic speeds and releasing that payload into the atmosphere.
As a result, MIRV technology has proven more attractive than MRV for advanced nations. Multiple-warhead missiles require both a miniaturized physics package and a lower mass re-entry vehicle, both of which are highly advanced technologies. As a result, single-warhead missiles are more attractive for nations with less advanced or less productive ...
The Vultee XA-41 was originally ordered as a dive bomber. After combat experience led the Army Air Corps to believe dive-bombers were too vulnerable to enemy fighters, the contract was amended to change the role to low-level ground attack. Although the XA-41 was a potent weapons system, the design was overtaken by more advanced technology, and ...
Data from Jane's All the World's Aircraft 2010/11 General characteristics Capacity: 2 Length: 6.35 m (41 ft 8 in) Wingspan: 9.60 m (63 ft 0 in) Height: 2.40 m (15 ft 8.94 in) Wing area: 11.60 m 2 (124.86 sq ft) gross Empty weight: 285 kg (628 lb) Max takeoff weight: 450 kg (992 lb) Fuel capacity: 75L Powerplant: 1 × Rotax 912 ULS 4-cylinder horizontally opposed liquid cooled piston, 75 kW ...
6 The DF-41 wasnt tested on september 25 as it says on the page. 1 comment. Toggle the table of contents. Talk: DF-41. Add languages.