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  2. SpaceX Super Heavy - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Super_Heavy

    The propellant tanks on Super Heavy are separated by a common bulkhead, similar to the ones used on the S-II and S-IVB stages on the Saturn V rocket [11] [12] After Starship's second flight test, the common dome's design was changed to a more elliptical dome, [13] which has changed the propellant capacity of both tanks by an unknown, but likely ...

  3. SpaceX Starship (spacecraft) - Wikipedia

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

    Block 2 ships will feature a new forward flap design, increased propellant capacity, and an increase in thrust. [327] Additionally, the leeward side of the vehicle has some external stringers. [328] These vehicles will be a total of 1.8 m (5 ft 11 in) meters taller than the previous Block 1 ships. [327

  4. Comparison of orbital launch systems - Wikipedia

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

    Falcon 9 Block 5, the most prolific active orbital launch system in the world.. This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit.

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  6. SpaceX Starship - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Starship

    SpaceX has stated that Starship, in its "baseline reuseable design", will have a payload capacity of 100–150 t (220,000–331,000 lb) to low earth orbit and 27 t (60,000 lb) to geostationary transfer orbit.

  7. Falcon Heavy - Wikipedia

    en.wikipedia.org/wiki/Falcon_Heavy

    The nominal payload capacity to a geostationary transfer orbit (GTO) is 8 t (18,000 lb) with recovery of all three first-stage cores (the price per launch is US$97 million), versus 26.7 t (59,000 lb) in fully expendable mode. The Falcon Heavy can also inject a 16 t (35,000 lb) payload into GTO if only the two side boosters are recovered.

  8. Table of specific heat capacities - Wikipedia

    en.wikipedia.org/wiki/Table_of_specific_heat...

    For example, Paraffin has very large molecules and thus a high heat capacity per mole, but as a substance it does not have remarkable heat capacity in terms of volume, mass, or atom-mol (which is just 1.41 R per mole of atoms, or less than half of most solids, in terms of heat capacity per atom).

  9. BelAZ 75710 - Wikipedia

    en.wikipedia.org/wiki/BelAZ_75710

    Carrying capacity, t 450 Gross weight, t 840,5 Body volume geometric, m³ 164,9 Body volume with a "cap" 2:1, m³ 268,3 Tires 59/80R63 Wheels 44,00—63/50 Suspension pneumohydraulic, shock absorber diameter - 1700 mm Fuel tank volume, l 2 х 2800 Fuel consumption, l/100 km 1300 Maximum speed, km/h 64 Powerplant Diesel engine model