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James Van Allen journal, 1951?-December 1954
Page 18
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"The Shock Tube: A Facility for Investigations in Fluid Dynamics" W. Bleakney, D.K. Weimer and C. H. Fletcher Review Sci Instr. 20, page 807 (1949) -------------------------------------------------------------- 2129 Pennsylvania Avenue Naval Reserve [Slingluff?] purchasing deal --------------------------------------------------------------- "Heat Transfer into the Nose Skin of the Bumper #5 Missile During Flight" B. R. L. Technical Note. Number 135 (November 1949) (Restricted) [sketch/picture] Drawing of rocket nose cone including: 1/16 inch steel, area of interest at 3.5 inches height down from tip [heat transfer detection point?], smaller cone tip appears reinforced] [sketch/picture] Graph of temperature versus flight time, with data peaks (680 degrees, over 585 degrees Fahrenheit; 80 seconds, 400 seconds) and valleys (0 degrees, 540 degrees; 0 seconds, 220 seconds), through temperatures of 500 degrees Fahrenheit absolute to 680 degrees Fahrenheit (absolute) and flight time from 0 seconds to 400 seconds, on Flight Date= 24 February 1949. [Vd?] maximum (110 seconds) 7500 feet/second
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"The Shock Tube: A Facility for Investigations in Fluid Dynamics" W. Bleakney, D.K. Weimer and C. H. Fletcher Review Sci Instr. 20, page 807 (1949) -------------------------------------------------------------- 2129 Pennsylvania Avenue Naval Reserve [Slingluff?] purchasing deal --------------------------------------------------------------- "Heat Transfer into the Nose Skin of the Bumper #5 Missile During Flight" B. R. L. Technical Note. Number 135 (November 1949) (Restricted) [sketch/picture] Drawing of rocket nose cone including: 1/16 inch steel, area of interest at 3.5 inches height down from tip [heat transfer detection point?], smaller cone tip appears reinforced] [sketch/picture] Graph of temperature versus flight time, with data peaks (680 degrees, over 585 degrees Fahrenheit; 80 seconds, 400 seconds) and valleys (0 degrees, 540 degrees; 0 seconds, 220 seconds), through temperatures of 500 degrees Fahrenheit absolute to 680 degrees Fahrenheit (absolute) and flight time from 0 seconds to 400 seconds, on Flight Date= 24 February 1949. [Vd?] maximum (110 seconds) 7500 feet/second
Van Allen Papers
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