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  2. Shuttle-Derived Heavy Lift Launch Vehicle - Wikipedia

    en.wikipedia.org/wiki/Shuttle-Derived_Heavy_Lift...

    A diagram of the Shuttle-Derived Heavy Lift Launch Vehicle, Block I configuration. The HLV was proposed to be a 4,600,000 pounds (2,100,000 kg) vehicle at liftoff with two 4-segment Space Shuttle Solid Rocket Boosters weighing about 2,600,000 pounds (1,200,000 kg) providing a total thrust of 5,900,000 pounds-force (26 MN) at sea level and the Space Shuttle External Tank weighing about ...

  3. Studied Space Shuttle designs - Wikipedia

    en.wikipedia.org/wiki/Studied_Space_Shuttle_designs

    The Heavy Lift Launch Vehicle was a study by NASA to turn the Space Shuttle launch stack into a dedicated uncrewed cargo launcher. The external tank and Space Shuttle Solid Rocket Boosters (SRBs) would be combined with a cargo module that took the place of the shuttle orbiter and included the Space Shuttle Main Engines.

  4. Shuttle-derived vehicle - Wikipedia

    en.wikipedia.org/wiki/Shuttle-Derived_Vehicle

    The Shuttle-C was a study by NASA to turn the Space Shuttle launch stack into a dedicated uncrewed cargo launcher. The Space Shuttle external tank and Space Shuttle Solid Rocket Boosters (SRBs) would be combined with a cargo module in place of the shuttle orbiter including the RS-25 engines. Various Shuttle-C concepts were investigated between ...

  5. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    All launch vehicle propulsion systems employed to date have been chemical rockets falling into one of three main categories: Solid-propellant rockets or solid-fuel rockets have a motor that uses solid propellants, typically a mix of powdered fuel and oxidizer held together by a polymer binder and molded into the shape of a hollow cylinder. The ...

  6. Comparison of retired orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_retired...

    Rocket 3.3 United States: Astra: 13.1 m 100 [65] 150 to SSO No 5 CCSFS, KLC: 2021 2022 Rokot-K Russia: Khrunichev: 25.5 m No 4 Baikonur, Plesetsk: 1990 1999 Rokot-KM Russia: Khrunichev: 29.1 m 1,950 [66] 1,200 to SSO No 31 Plesetsk: 2000 2019 RS1 B1 United States: ABL Space Systems: 27 m 1,350 [67] 400: 975 to SSO 750 to MEO No 1 KLC: 2023 [68 ...

  7. Comparison of satellite buses - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_satellite_buses

    power range 3–18 kW in four sub-models TubeSat Kit [11] United States Interorbital Systems: 0.5 kg 0.75 kg 0.008 [12] 0 Development LEO CubeSat Kit [4] United States Pumpkin Inc. 1.65 kg 3 kg 0.194 [13] 23: Operational 2007 2012 LEO; CubeSat GOMX [14] Denmark: GomSpace: 1.50 kg 3 kg 1: Operational 2013 2013 LEO; DFH-3: China: China Academy of ...

  8. Space Launch System - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System

    Development of SLS began in 2011 as a replacement for the retiring Space Shuttle as well as the canceled Ares I and Ares V launch vehicles. SLS was built using existing Shuttle technology, including solid rocket boosters and RS-25 engines. The rocket has been criticized for its political motivations, seen as a way to preserve jobs and contracts ...

  9. List of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/List_of_orbital_launch_systems

    Comparison of Saturn V, Space Shuttle, three Ares rockets, and SLS Block 1 Titan rockets. Ares – Canceled. Ares I; Ares IV; Ares V; Astra Space launch vehicles. Rocket 3 – Retired; Rocket 4 – Under development; Athena – Retired. Athena I; Athena II; Atlas. Atlas B – Retired; Atlas D – Retired; Atlas-Able – Retired; Atlas-Agena ...

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