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  2. Irtysh (rocket) - Wikipedia

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

    Irtysh (Russian: Иртыш), [2] also named Soyuz-5 (Russian: Союз-5), formerly codenamed Fenix in Russian and Sunkar (Kazakh: Сұңқар, lit. ' falcon ') in Kazakh, is a planned Russian rocket that is being developed by RKTs Progress within the "Project Feniks" ( Russian : Феникс , lit.

  3. Soyuz 5 - Wikipedia

    en.wikipedia.org/wiki/Soyuz_5

    Leonov served as a consultant for the design process, which was completed during 1966. Suit fabrication and testing occurred in 1967, but the Soyuz 1 accident in April of that year and Soyuz docking difficulties on the Soyuz 2 and Soyuz 3 missions delayed their use in space until the Soyuz 4 and Soyuz 5 flights. To prevent the suit from ...

  4. Soyuz 2.1v - Wikipedia

    en.wikipedia.org/wiki/Soyuz_2.1v

    The Soyuz‑2.1v was designed to serve lighter payloads with a payload capacity of 2,850 kg (6,280 lb) to a 200 km (120 mi) circular low Earth orbit with an inclination of 51.8° from Baikonur, and 2,800 kg (6,200 lb) to a 200 kilometre orbit at 62.8° from Plesetsk.

  5. Plesetsk Cosmodrome Site 43 - Wikipedia

    en.wikipedia.org/wiki/Plesetsk_Cosmodrome_Site_43

    As of 2024, both pads remain in use for the Soyuz-2.1a and Soyuz-2.1b rockets. Additionally, Site 43/4 also hosts launches of the smaller Soyuz-2.1v launch vehicle. Originally constructed for the R-7A Semyorka missiles, the site hosted its first launch on 21 December 1965, when an R-7A test flight was conducted from Site 43/3. The first launch ...

  6. RD-0124 - Wikipedia

    en.wikipedia.org/wiki/RD-0124

    It is the version for the Soyuz 2.1b and Soyuz 2.1v Block I stage. It is the first liquid rocket engine designed in Russia after the Soviet period. [3] [citation needed] RD-0124A It is the version that powers the Angara URM-2, both the 1.2 and the bigger 5 versions. It differs on the base model in having an extended burn time of 424 seconds and ...

  7. Comparison of orbital launch systems - Wikipedia

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

    [note 2] Liquid-propellant rockets have a motor that feeds liquid propellant(s) into a combustion chamber. Most liquid engines use a bipropellant , consisting of two liquid propellants (fuel and oxidizer) which are stored and handled separately before being mixed and burned inside the combustion chamber.

  8. List of Soyuz missions - Wikipedia

    en.wikipedia.org/wiki/List_of_Soyuz_missions

    The first era of the Soyuz programme's crewed missions (Soyuz 1-40) used the 7K series of Soyuz craft, which included the first-generation (1.0) Soyuz 7K-OK, a variant (1.5) Soyuz 7K-OKS, the second-generation (2.0) Soyuz 7K-T, and the (2.5) Soyuz 7K-TM variant. Following this first era, successive eras of crewed missions have had mission ...

  9. Soyuz (rocket) - Wikipedia

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

    It was commissioned to launch Soyuz spacecraft as part of the Soviet human spaceflight program, first with eight uncrewed test flights, followed by the first 19 crewed launches. [1] The original Soyuz also propelled four test flights of the improved Soyuz 7K-T capsule between 1972 and 1974. It flew 30 successful missions over ten years and ...