Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet Page: 1 of 89
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Bureau of Aeronautics, Department of the Navy
PRELIMINARY PERFORMANCE DATA FOR THE J57-P- TURBOJET
ENGINE AT ALTITUDES UP TO 65,000 FEET
By Robert R. Miller and Harry E. Bloomer
L.ewis- Flight Propulsion Laboratory
C level d, Ohio
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This material contains information affecting the National Defense of the United States within the meaning
of the espionage laws, Title 18, U.S.C., Secs. 793 and 794, the transmission or revelation of which in any
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NATIONAL ADVISORY COMMITTEE,
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Miller, Robert R. & Bloomer, Harry E. Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet, report, June 15, 1954; (digital.library.unt.edu/ark:/67531/metadc60049/m1/1/: accessed February 21, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.