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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.
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 ...
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.
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 ...
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 ...
[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.
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 ...
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 ...