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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. 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 ...

  4. 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.

  5. Space Shuttle design process - Wikipedia

    en.wikipedia.org/wiki/Space_Shuttle_design_process

    The primary intended use of the Phase A Space Shuttle was supporting the future space station, ferrying a minimum crew of four and about 20,000 pounds (9,100 kg) of cargo, and being able to be rapidly turned around for future flights, with larger payloads like space station modules being lifted by the Saturn V.

  6. Martin Marietta X-24 - Wikipedia

    en.wikipedia.org/wiki/Martin_Marietta_X-24

    The X-24B's design evolved from a family of potential reentry shapes, each with higher lift-to-drag ratios, proposed by the Air Force Flight Dynamics Laboratory.To reduce the costs of constructing a research vehicle, the Air Force returned the X-24A to the Martin Marietta Corporation (as Martin Aircraft Company became after a merger) for modifications that converted its bulbous shape into one ...

  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. Comparison of orbital rocket engines - Wikipedia

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

    Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio

  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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