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A super heavy-lift launch vehicle is a rocket that can lift to low Earth orbit a "super heavy payload", which is defined as more than 50 metric tons (110,000 lb) [1] [2] by the United States and as more than 100 metric tons (220,000 lb) by Russia. [3]
The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.
A heavy-lift launch vehicle (HLV) is an orbital launch vehicle capable of lifting payloads between 20,000 to 50,000 kg (44,000 to 110,000 lb) (by NASA classification) or between 20,000 to 100,000 kilograms (44,000 to 220,000 lb) (by Russian classification) [1] into low Earth orbit (LEO). [2]
A 1 m (3 ft 3 in) and a 1.7 m (5 ft 7 in) tall ring are used to construct the liquid oxygen header tank. These rings have a significantly smaller diameter than the main rings. [47] The forward dome is constructed out of two segments: the "dome knuckle" and the "dome frustum".
Yenisei (Russian: Енисей), project name RN STK-1 (Raketa-Nositel' SverkhTyazhologo Klassa - Carrier rocket super-heavy class), is a super-heavy launch vehicle being developed by the Russian space industry.
[3] When the final approach isn't stabilised, the crew is to abort and go around; this was the recommendation of the Australian Transport Safety Bureau after investigating the hard landing of a Malaysia Airlines Airbus A330 at Melbourne Airport after arriving from Kuala Lumpur on 14 March 2015. [4] [5]
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