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  2. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    The Saturn V [f] is a retired ... The size and payload capacity of the Saturn V dwarfed those of all other previous rockets successfully flown at that time. With the ...

  3. Payload fraction - Wikipedia

    en.wikipedia.org/wiki/Payload_fraction

    The payload fraction is the quotient of the payload mass and the total vehicle mass at the start of its journey. ... Apollo 17 Saturn V [3] 2,961,860 kg 48,609 kg to ...

  4. Super heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Super_heavy-lift_launch...

    The final launch of Saturn V in 1973 placed Skylab, a 77-tonne (170,000 lb) payload, into LEO. The Energia launcher was designed by the Soviet Union to launch up to 105 t (231,000 lb) to low Earth orbit. [ 8 ]

  5. Comparison of orbital launch systems - Wikipedia

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

    Maximum payload mass (kg) Reusable / Expendable Orbital launches including failures [a] Suborbital test flights Launch site(s) Dates of flight LEO GTO Other First Latest Starship Block 1 [140] United States: SpaceX: 121 m 40,000 – 50,000 [141] N/A N/A Reusable: 0 6 Starbase: 2023 2024 Angara A5 / Orion Russia: Khrunichev: 54.9 m N/A 6,500 ...

  6. Saturn V ELV - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_ELV

    A 1968 proposal for a Saturn V ELV (MLV-SAT-V-25(S)U) According to the 1968 NASA document "Integrated Manned Interplanetary Spacecraft Concept Definition", there was a planned schedule for exploration under the ELV program. [2] After the first crewed Apollo lunar landing, NASA was hoping to progress through the following list:

  7. N1 (rocket) - Wikipedia

    en.wikipedia.org/wiki/N1_(rocket)

    The N1-L3 would have been able to convert only 9.3% of its three-stage total impulse into Earth orbit payload momentum (compared to 12.14% for the Saturn V), and only 3.1% of its four-stage total impulse into translunar payload momentum, compared to 6.2% for the Saturn V. The Saturn V also never lost a payload in two development and eleven ...

  8. Marshall Space Flight Center - Wikipedia

    en.wikipedia.org/wiki/Marshall_Space_Flight_Center

    Designed under the direction of Arthur Rudolph, the Saturn V holds the record as the largest and most powerful launch vehicle ever brought to operational status from a combined height, weight, and payload standpoint. The Saturn V consisted of three propulsion stages and an instrument unit.

  9. Crawlerway - Wikipedia

    en.wikipedia.org/wiki/Crawlerway

    The Crawlerway was originally designed to support the weight of the Saturn V rocket and its payload, plus the Launch Umbilical Tower and mobile launcher platform, atop a crawler-transporter during the Apollo program. It was also used from 1981 to 2011 to transport the lighter Space Shuttles to their launch pads.