1. Rocket engines turbopumps designed by NPO Energomash;chvanov;Konversiya v mashinostroenii,2006
2. Development of turbopump for modern oxygen-kerosene engines with oxidizer-rich staged combustion cycle;dmitrenko;Kosmonavtika,2012
3. Features of the development of an oxidizing gas generator for a multi-mode single-chamber engine;adzhyan;Trudy NPO Energomash,2010
4. Features of RD-120 engine forcing investigation;katorgin;Vestnik otdeleniya “Kosmicheskic energeticheskie sistemy novogo pokoleniya” Rossijskoj akademii kosmonavtiki im K E Tsiolkovskogo,2004