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  2. N1 (rocket) - Wikipedia

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

    The N1/L3 (from Ракета-носитель Raketa-nositel', "Carrier Rocket"; Cyrillic: Н1) [5] was a super heavy-lift launch vehicle intended to deliver payloads beyond low Earth orbit. The N1 was the Soviet counterpart to the US Saturn V and was intended to enable crewed travel to the Moon and beyond, [6] with studies beginning as early ...

  3. File:N-1 L3 lunar mission profile.svg - Wikipedia

    en.wikipedia.org/wiki/File:N-1_L3_lunar_mission...

    Use of NASA logos, insignia and emblems is restricted per U.S. law 14 CFR 1221.; The NASA website hosts a large number of images from the Soviet/Russian space agency, and other non-American space agencies.

  4. Super heavy-lift launch vehicle - Wikipedia

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

    The only Universal Rocket to make it past the design phase was the UR-500 while the N1 was selected to be the Soviets' HLV for lunar and Martian missions. [65] The UR-900, proposed in 1969, would have had a payload capacity of 240 t (530,000 lb) to low earth orbit. It never left the drawing board. [66]

  5. NK-33 - Wikipedia

    en.wikipedia.org/wiki/NK-33

    Documentary video on Russian rocket engine development of the NK-33 and its predecessors for the N1 rocket. (NK-33 story starts at 24:15–26:00 (program shuttered in 1974); the 1990s resurgence and eventual sale of the remaining engines from storage starts at 27:25; first use on a US rocket launch in May 2000.) NK-33's specifications

  6. N-I (rocket) - Wikipedia

    en.wikipedia.org/wiki/N-I_(rocket)

    Mock up of N-1. The N-I or N-1 was a derivative of the American Thor-Delta rocket, produced under license in Japan. The N stood for "Nippon" (Japan). It used a Long Tank Thor first stage, a Mitsubishi Heavy Industries-designed LE-3 engine on the second stage, [3] [4] [5] and three Castor SRMs.

  7. RD-270 - Wikipedia

    en.wikipedia.org/wiki/RD-270

    The RD 270 was also considered for the R-56 rocket (although never formally adopted) until work on the design stopped in June 1964. [2] [3] During development, Glushko studied the use of Pentaborane propellants in a modified RD-270M engine. This would have created immense toxicity problems but increased the specific impulse of the engine by 42 ...

  8. Baikonur Cosmodrome Site 110 - Wikipedia

    en.wikipedia.org/wiki/Baikonur_Cosmodrome_Site_110

    It was followed by the left (or west) pad, called "110/37" or "110L". The complex was built in the 1960s as part of the Soviet crewed lunar programs, for use by the N1 rocket. [citation needed] A total of five launches were made from the complex: Four N1 launches as well as one Energia launch, carrying the Buran spaceplane.

  9. Blok D - Wikipedia

    en.wikipedia.org/wiki/Blok_D

    Blok D (Russian: Блок Д, lit. 'Block D') is an upper stage used on Soviet and later Russian expendable launch systems, including the N1, Proton-K and Zenit. [2]The stage (and its derivatives) has been included in more than 320 launched rockets as of 2015. [3]