R-28 Sarmat ("Satan 2") ICBM Flight History by Variant/Year (2022- ) Page 1 of 1: L(F) = Number of Launches(Number of Failures) RS-28 ICBM* Year L(F) L(F) L(F) L(F) L(F) L(F) L(F) L(F) --------------------------------------------------------------------- 2020 - - - - - - - - 2021 - - - - - - - - 2022 1(0) - - - - - - - 2023 1(1) - - - - - - - --------------------------------------------------------------------- RS-28 ICBM* L(F) L(F) L(F) L(F) L(F) L(F) L(F) L(F) --------------------------------------------------------------------- Suborb 2(1) - - - - - - - Orbit - - - - - - - - Total 2(1) - - - - - - - --------------------------------------------------------------------- Footnotes: * Suborbital Flights RS-28 Flight History --------------------------------------------------------------------- 04/20/22 RS-28 Sarmat ICBM Test PL SUB 02/18/23 RS-28 Sarmat ICBM Test PL [FSO][2] --------------------------------------------------------------------- [2] Possible guidance and control failure during second stage operation. RS-28 Description RS-28 Sarmat is a three-stage liquid fueled ICBM. It measures 3.0 x 35.5 meters. It weighes 208.1 tonnes at launch from its silo. It is believed derived from R-36M ICBM family. It has 10 tonne payload and 10,000-18,000 km range. N2O4/UDMH. First stage powered by RD-274 (4xRD-273) engines. 1,113,253 lbf S/L. ISP 296 sec S/L. Jonathan's Space Report Launch Vehicle Database "http://www.planet4589.org/space/lvdb/index.html" Encylopedia Astronautica "http://www.astronautix.com/" Gunter's Space Page "http://www.skyrocket.de/space" Last Update 12/31/2023 by Ed Kyle