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  2. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    If all three stages were to explode simultaneously on the launch pad, an unlikely event, the Saturn V had a total explosive yield of 543 tons of TNT or 0.543 kilotons (2,271,912,000,000 J or 155,143 lbs of weight loss), which is 0.222 kt for the first stage, 0.263 kt for the second stage and 0.068 kt for the third stage. [76]

  3. S-IC-T - Wikipedia

    en.wikipedia.org/wiki/S-IC-T

    S-IC-T was planned as a test rocket only and not to be used in the later Apollo program. The Saturn V rocket was used in the Apollo program to depart Earth's gravity. S-IC-T, like all following Saturn V's S-IC rockets used five Rocketdyne F-1 engines. The Rocketdyne F-1 engine was first tested in March 1959 and delivered to NASA in October 1963.

  4. 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:

  5. Saturn (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Saturn_(rocket_family)

    The Saturn C-5 (later given the name Saturn V), the most powerful of the Silverstein Committee's configurations, was selected as the most suitable design. At the time the mission mode had not been selected, so they chose the most powerful booster design in order to ensure that there would be ample power. [ 24 ]

  6. Super heavy-lift launch vehicle - Wikipedia

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

    The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [69] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [ 70 ] Nova was cancelled in 1964 and had reusable ...

  7. S-IC - Wikipedia

    en.wikipedia.org/wiki/S-IC

    The S-IC (pronounced S-one-C [3] [4]) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, more than 90% of the mass at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer.

  8. NASCAR Cup Series 2025 schedule: Tracks, dates, times, how to ...

    www.aol.com/nascar-cup-series-2025-schedule...

    The NASCAR Cup Series returns in early February to begin its 2025 season.. The season kicks off with The Clash exhibition race, which moves to Bowman Gray Stadium in Winston-Salem, North Carolina ...

  9. Medium-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Medium-lift_launch_vehicle

    The first US medium-lift vehicle was a purpose-built orbital launch vehicle, the Saturn I. Saturn I first launched in 1961, and the Saturn family would eventually grow into the heavy-lift Saturn IB and the super-heavy lift Saturn V. [4] ICBM-derived launch vehicles for the US include the Atlas, Titan, and Delta families.