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S5.98M
Russian rocket engine

The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages. It was designed by KB KhIMMASH, the famous Isaev designed bureau. It burns a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer in a gas-generator cycle.

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See also

  • Briz-M - The upper stage that is powered by the S5.98M.
  • Proton-M - The heavy lift rocket that uses the Briz-M stage.
  • Rokot - The light lift rocket that uses the smaller Briz-KM stage.
  • Khrunichev - The manufacturer of the Briz stage and the corporate parent of the designer bureau.

References

  1. Zak, Anatoly (2014-11-06). "Briz upper stage". RussianSpaceWeb.com. Retrieved 2015-09-03. http://www.russianspaceweb.com/briz.html

  2. "Breeze M Upper Stage". khrunichev.ru. Khrunichev State Research and Production Space Center. Archived from the original on 3 June 2015. https://web.archive.org/web/20150603011250/http://www.khrunichev.ru/main.php?id=49&lang=en

  3. Rockot User's Guide (PDF). EUROCKOT Launch Services GmbH. April 2011. Retrieved 2015-09-03. http://www.eurockot.com/wp-content/uploads/2012/10/UsersGuideIss5Rev0web.pdf

  4. "КБХМ им.А.М.Исаева - Двигатель 14Д30. Разгонный блок "Бриз-М"" [Engine 14D30. The upper stage «Briz-M»]. kbhmisaeva.ru. KB KhIMMASH. Archived from the original on 23 April 2013. https://web.archive.org/web/20130423190142/http://kbhmisaeva.ru/main.php?id=52

  5. Brügge, Norbert. "Spacecraft-propulsion blocks from Isayev Design bureau (Khimmash)". b14643.de. Archived from the original on 2 June 2015. Retrieved 19 June 2015. https://web.archive.org/web/20150602231608/http://www.b14643.de/Spacerockets/Diverse/KB-Isayev_KDUs/index.htm

  6. "Конструкторское бюро химического машиностроения имени А.М.Исаева (КБХМ)" [Chemical Engineering Design Bureau name after A.M.Isaev (KBHM)]. lpre.de. Retrieved 22 June 2017. http://lpre.de/kbhm/index.htm