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  2. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock ...

  3. Steve Eves - Wikipedia

    en.wikipedia.org/wiki/Steve_Eves

    The rocket was 36 feet (11 m) tall and weighed 1,648 pounds (748 kg). [1] On Saturday April 25, 2009 Eves launched the 1/10 scale replica of the Saturn V rocket 4,441 feet (1,354 m) into the air, and successfully recovered it. [ 2 ]

  4. Comparison of crewed space vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_crewed_space...

    Payload (kg) ‡ First spaceflight § Last spaceflight Flights § Mercury ... Saturn IB Saturn V: 3: 8.5: 3.91: 5,500 CM + 14,700 LM + 24,500 Service Module: Fuel cells

  5. Talk:Saturn V/Archive 1 - Wikipedia

    en.wikipedia.org/wiki/Talk:Saturn_V/Archive_1

    The LEO orbital payload of the Saturn V which launched Skylab was 147,363 kg. Of this about 36,500 kg was the non-functional dry mass of the SII 2nd stage. Total orbital mass of the Skylab workshop was about 88,474 kg. Various other sources state the Saturn V LEO payload as 118,000 kg . So there are various ways to define payload: total ...

  6. S-V - Wikipedia

    en.wikipedia.org/wiki/S-V

    The S-V would ultimately fly as the third stage on early launches of the Saturn I. Convair delivered two S-V stages in February 1961 [1] with one being flown on SA-1 attached to an also inert S-IV, the second was used for dynamic testing of the complete Saturn I before being later flown. In May 1961 NASA eliminated the requirement for all ...

  7. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    During their two and a half minutes of operation, the five F-1s propelled the Saturn V vehicle to a height of 42 miles (222,000 ft; 68 km) and a speed of 6,164 mph (9,920 km/h). The combined flow rate of the five F-1s in the Saturn V was 3,357 US gal (12,710 L) [5] or 28,415 lb (12,890 kg) per second.

  8. Cheap and deadly: Why vehicle terror attacks like the Bourbon ...

    www.aol.com/cheap-deadly-why-vehicle-terror...

    According to the Associated Press/USA TODAY/Northeastern University Mass Killing Database, before the New Orleans attack there had been three intentional and indiscriminate vehicle rammings since ...

  9. 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 ...