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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. 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. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list ...

  4. Comparison of orbital launcher families - Wikipedia

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

    A Saturn V rocket, one of the most powerful operational launch vehicles to date. This article compares different orbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries).

  5. 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 ]

  6. Space Launch System - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System

    In September 2012, an SLS deputy project manager stated that $500 million is a reasonable target average cost per flight for the SLS program. [67] In 2013, the Space Review estimated the cost per launch at $5 billion, depending on the rate of launches.

  7. Launch Vehicle Digital Computer - Wikipedia

    en.wikipedia.org/wiki/Launch_Vehicle_Digital...

    Boeing, Saturn V Launch Vehicle Guidance Equations, SA-504, 15 July 1967; Haeussermann, Walter (July 1970). Description and Performance Of The Saturn Launch Vehicle's Navigation, Guidance And Control System (PDF). NASA TN D-5869. NASA Marshall Spaceflight Center, Saturn V Flight Manual SA-503, 1 November 1968

  8. Apollo program - Wikipedia

    en.wikipedia.org/wiki/Apollo_program

    Saturn V launch vehicles and flights were designated with an AS-500 series number, "AS" indicating "Apollo Saturn" and the "5" indicating Saturn V. [67] The three-stage Saturn V was designed to send a fully fueled CSM and LM to the Moon. It was 33 feet (10.1 m) in diameter and stood 363 feet (110.6 m) tall with its 96,800-pound (43,900 kg ...

  9. Saturn V ELV - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_ELV

    The Saturn V-ELV (Earth Launch Vehicle) was to be an enlarged Saturn V with the addition of four UA1207 [1] ... First crewed hyperbolic reentry at 65k feet per second.