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  2. Proton-M - Wikipedia

    en.wikipedia.org/wiki/Proton-M

    This was the 326th launch of a Proton, the 16th Proton-M/Briz-M launch, and the 41st Proton launch to be conducted by ILS. [13] It features more efficient first stage engines, updated avionics, lighter fuel tanks and more powerful vernier engines on the Briz-M upper stage, and mass reduction throughout the rocket, including thinner fuel tank ...

  3. Blok DM-03 - Wikipedia

    en.wikipedia.org/wiki/Blok_DM-03

    As of September 2015, 3 Proton-M/Blok DM-03 have been launched, of which 2 have failed. In the 2010 failure, the rocket was too heavy to reach orbit and reentered the atmosphere during a coast phase between the end of third stage flight and the beginning of the Blok DM-03's first burn, whilst the 2013 flight failed after the rocket went out of ...

  4. Comparison of orbital launcher families - Wikipedia

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

    Any orbit (regardless of outcome): Flights which achieve at least one complete orbit even if the orbit differs from the targeted orbit. Target orbit (without damage to the payload) Status: Actual status of launcher (retired, development, active) Date of flight First: Year of first flight of first family member

  5. CORRECTING and REPLACING ILS Proton Successfully ... - AOL

    www.aol.com/news/2013-03-27-correcting-and...

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  6. Heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Heavy-lift_launch_vehicle

    The first heavy-lift launch vehicles in the 1960s included the US Saturn IB and the Soviet Proton family. Saturn IB was designed to carry the Apollo spacecraft into orbit and had increased engine thrust and a redesigned second stage from its predecessor. Proton was originally designed to be a large intercontinental ballistic missile (ICBM). [4]

  7. Briz (rocket stage) - Wikipedia

    en.wikipedia.org/wiki/Briz_(rocket_stage)

    A Proton with a Briz-M can place a 4,385 kg satellite, such as an A2100AX, into a target orbit with an apogee of 35,786 km, a perigee of 7,030 km, and an inclination of 17.3°. [ 9 ] [ 10 ] Maximum lift capability of the Briz-M stage is 5,645 kg to geosynchronous transfer orbit with a 1,500 m/s residual velocity to GSO. [ 6 ]

  8. Comparison of orbital launch systems - Wikipedia

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

    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 includes all upcoming rockets.

  9. AOL Mail for Verizon Customers - AOL Help

    help.aol.com/products/aol-mail-verizon

    AOL Mail welcomes Verizon customers to our safe and delightful email experience!