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Docking of two vehicles in space has previously only been achieved by the Soviet Union/Russia, United States, ESA, and China. Kuiper Systems , Amazon's satellite internet subsidiary, plans to ramp up launches for its constellation of over 3,000 satellites.
Any orbit (regardless of outcome): Flights which achieve at least one complete orbit even if the orbit differs from the targeted orbit. Target orbit (without damage to the payload) Status: Actual status of launcher (retired, development, active) Date of flight First: Year of first flight of first family member
On 9 March 2021, China and Russia signed a “Memorandum of Understanding between the Government of the People’s Republic of China and the Government of the Russian Federation Regarding Cooperation for the Construction of the International Lunar Research Station.” [14] On 16 June 2021, Roscosmos and the China National Space Administration (CNSA) held a joint session in St. Petersburg ...
Lists of orbital launch vehicles by payload capacity: Small-lift launch vehicle (up to 2,000 kg to Low Earth Orbit (LEO)) Medium-lift launch vehicle (from 2,000 to 20,000 kg to LEO) Heavy-lift launch vehicle (from 20,000 to 50,000 kg to LEO) Super heavy-lift launch vehicle (beyond 50,000 kg to LEO)
A launch service provider is a type of company that uses launch vehicles and related services provided by a Launch Agency, including furnishing the launch vehicles, launch support, equipment and facilities, for the purpose of launching satellites into orbits or deep space. [1]
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 medium-lift launch vehicle (MLV) is a rocket launch vehicle that is capable of lifting between 2,000 to 20,000 kg (4,400 to 44,100 lb) by NASA classification or between 5,000 to 20,000 kilograms (11,000 to 44,000 lb) by Russian classification [1] of payload into low Earth orbit (LEO). [2]
The Soyuz‑2.1v was designed to serve lighter payloads with a payload capacity of 2,850 kg (6,280 lb) to a 200 km (120 mi) circular low Earth orbit with an inclination of 51.8° from Baikonur, and 2,800 kg (6,200 lb) to a 200 kilometre orbit at 62.8° from Plesetsk.