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Reusable super-heavy rocket 2 Deep space Testing (2/4) 2023 Stoke Space: Nova Reusable light rocket 2 LEO Development Unknown [152] Success Rockets: Nebo 1: Ultralight rocket 1 Suborbital Operational (1/1) December 2021 [153] Stalker: Ultralight rocket 2 LEO Development 2024 [154] United Launch Alliance: Atlas V: Medium rocket 2 + 0-5 boosters TMI
Nova is a fully reusable medium-lift launch vehicle being developed by Stoke Space. [16] Announced in October 2023, [17] Stoke Space plans to use two stages with an expected payload capacity of 5 tons (5,000 kg) to low Earth orbit (), with the first stage performing a return-to-launch-site (RTLS) landing.
During this period, no commercial space launches were available to private operators, and no private organization was able to offer space launches. In the 1980s, the European Space Agency created Arianespace , the world's first commercial space transportation company, and, following the Challenger disaster , the American government deregulated ...
ABL Space Systems was founded in 2017 by Harry O'Hanley and Dan Piemont, former SpaceX and Morgan Stanley employees. Their RS-1 rocket has two stages. It offers a maximum capacity of 1,350 kg (2,980 lb) to low Earth orbit (LEO). [3] In 2018, ABL Space Systems signed a lease with Camden County, Georgia, for future operations in Spaceport Camden. [4]
Rocket 4 is a new rocket design, improving on capability and reliability compared to the outgoing Rocket 3 series. 18.9 m (62 ft) in height and 1.8 m (5.9 ft) in diameter, its planned payload capacity is 550 kg to a 300 km low Earth orbit or 350 kg to a 500 km sun-synchronous orbit.
That is until Rocket Lab (NASDAQ: RKLB) joined the party. Nipping at SpaceX's heels, Rocket Lab has built a successful niche in the space economy and is now the second private space flight company ...
The Aeon R engine, currently under development, is a high pressure gas generator cycle LOX/subcooled Methane propellants engine [35] designed to produce 258,000 lbf (1,150 kN) of thrust at sea level and 279,000 lbf (1,240 kN) in a vacuum. 13 Aeon R engines will power the first stage of Terran R with a combined liftoff thrust of 3,354,000 lbf.
A new feature for the engine is the ability to throttle from 100% to 70%. [7] The engine's 150:1 thrust-to-weight ratio is the highest ever achieved for a rocket engine. [8] [9] The first flight of the Merlin 1D engine was also the maiden Falcon 9 v1.1 flight. [10]
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