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  2. Space Launch System - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System

    The Space Launch System ( SLS) is an American super heavy-lift expendable launch vehicle used by NASA. As the primary launch vehicle of the Artemis Moon landing program, SLS is designed to launch the crewed Orion spacecraft on a trans-lunar trajectory. The first SLS launch was the uncrewed Artemis 1, which took place on 16 November 2022.

  3. Shuttle-Derived Heavy Lift Launch Vehicle - Wikipedia

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

    The Shuttle-Derived Heavy Lift Launch Vehicle (" HLV ") was an alternate super heavy-lift launch vehicle proposal for the NASA Constellation program. It was first presented to the Augustine Commission on 17 June 2009. Based on the Shuttle-C concept which has been the subject of various studies since the 1980s, the HLV was a Shuttle-Derived ...

  4. Single-stage-to-orbit - Wikipedia

    en.wikipedia.org/wiki/Single-stage-to-orbit

    The VentureStar was a proposed SSTO spaceplane. A single-stage-to-orbit ( SSTO) vehicle reaches orbit from the surface of a body using only propellants and fluids and without expending tanks, engines, or other major hardware. The term usually, but not exclusively, refers to reusable vehicles. [1] To date, no Earth-launched SSTO launch vehicles ...

  5. Next Generation Launch Vehicle - Wikipedia

    en.wikipedia.org/wiki/Next_Generation_Launch_Vehicle

    Next Generation Launch Vehicle. The Next Generation Launch Vehicle or NGLV (previously referred to as Unified Launch Vehicle or ULV) is a three-stage partially reusable rocket, currently under development by the Indian Space Research Organisation (ISRO). This vehicle is designed to replace currently operational systems like PSLV, GSLV and LVM3.

  6. Orion (spacecraft) - Wikipedia

    en.wikipedia.org/wiki/Orion_(spacecraft)

    Orion ( Orion Multi-Purpose Crew Vehicle or Orion MPCV) is a partially reusable crewed spacecraft used in NASA 's Artemis program. The spacecraft consists of a Crew Module (CM) space capsule designed by Lockheed Martin and the European Service Module (ESM) manufactured by Airbus Defence and Space. Capable of supporting a crew of four beyond low ...

  7. Space Launch System core stage - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System_core_stage

    LH 2 / LOX. The Space Launch System core stage, or simply core stage, is the main stage of the American Space Launch System (SLS) rocket, built by The Boeing Company in the NASA Michoud Assembly Facility. At 65 m (212 ft) tall and 8.4 m (27.6 ft) in diameter, the core stage contains approximately 987 t (2,177,000 lb) of its liquid hydrogen and ...

  8. StarTram - Wikipedia

    en.wikipedia.org/wiki/StarTram

    StarTram is a proposed space launch system propelled by maglev technology. The initial Generation 1 facility is proposed to launch cargo only from a mountain peak at an altitude of 3 to 7 kilometres (9,800 to 23,000 ft) using an evacuated tube remaining at local surface level. Annual orbital lift was estimated at approximately 150,000 tons.

  9. Space Shuttle Solid Rocket Booster - Wikipedia

    en.wikipedia.org/wiki/Space_Shuttle_Solid_Rocket...

    Burn time. 127 s. Propellant. PBAN - APCP. The Space Shuttle Solid Rocket Booster ( SRB) was the first solid-propellant rocket to be used for primary propulsion on a vehicle used for human spaceflight. [1] A pair of these provided 85% of the Space Shuttle 's thrust at liftoff and for the first two minutes of ascent.