INDUSTRIAL USE OF ULTRASOUND (SELECTED PART)
Abstract
Aerospace Technical Intelligence Center, WrightPatterson Air Force Base, Ohio. THEORY AND DESIGN OF PUMPS FOR LIQUID-FUEL ROCKET ENGINES (Teoriya I Raschet Nasosov Zhidkostnykh Raketnykh Dvigateley), by B. V. Ovsyannikov. 23 May 61, 312p. incl. illus. tables, 28 refs. (Trans. no. MCL-841 of Gosudarstvennoye Nauchno-T AD-261 780Div. 27U (22 Aug 61) OTS price $19. 75Aerospace Technical Intelligence Center, WrightPatterson Air Force Base, Ohio. THEORY AND DESIGN OF PUMPS FOR LIQUID-FUEL ROCKET ENGINES (Teoriya I Raschet Nasosov Zhidkostnykh Raketnykh Dvigateley), by B. V. Ovsyannikov. 23 May 61, 312p. incl. illus. tables, 28 refs. (Trans. no. MCL-841 of Gosudarstvennoye Nauchno-Tekhnicheskoye Izdatel'stvo Oboronigiz, Moscow, 247p., 1960) Unclassified report DESCRIPTORS: *Rocket motors, Fuel systems, *Fuel pumps, Liquid rocket propellants, Rocket fuels, *Centrifugal pumps, Rotary pumps, Design, Theory, Rocket propulsion, USSR, Bib liography, *Textbooks. This publication was designed as a textbook for students and engineers on the theory and design of pumps for liquid-fuel rocket engines. Topics include: applications of pumps in liquid rocket fuel systems; basic concepts pertaining to ZhRD centrifugal pumps and cavitation in centrifugal pumps for ZhRD; efficiencies of centrifugal pumps; operation, characteristics and design of centrifugal pumps; and concise information on existing ZhRD pumps.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 26, 1961
- Accession Number
- AD0261779
Entities
Organizations
- National Air and Space Intelligence Center