Abstract
2 Sturm, E. J. and Reichenbach, R. E., Aluminized Composite Solid-Propellant Burning Rates in Acceleration Fields, AIAA Journal, Vol. 7, No. 11, Nov. 1969, pp. 2087-2093. 3 Manda, L. J., Compilation of Rocket Spin Data, Vol. II: Literature Survey, Rept. 3001-2, CR-66641, 1968, NASA. 4 Anderson, J. B. and Reichenbach, R. E., '76-Inch Diameter Centrifuge Facility, TN 66T-4, Sept. 1966, Dept. of Aeronautics, Naval Postgraduate School, Monterey, Calif. 5 Sturm, E. J., A Study of the Burning Rates of Composite Solid Propellants in Acceleration Fields, Ph.D. thesis, AD832206, March 1968, Naval Postgraduate School, Monterey, Calif. 6 Green, L., Jr., Burning of Some Composite Solid Propellants, Jet Propulsion, Vol. 24, No. 1, Jan-Feb. 1954 DD 9-15. ' 7 Wimpress, R. N., Internal Ballistics of Solid Fuel Rockets, 1st ed., McGraw-Hill, New York, 1950. 8 Lawrence, W. J. and Deverall, L. L, The Erosive Burning Behavior of Selected Composite Propellants, Proceedings from the 4th ICRPG Combustion Conference, Stanford Research Inst., Menlo Park, Calif., Oct. 1967, pp. 459-466. 9 Crump, J., Aluminum Combustion in Composite Propellants, Proceedings of the Second ICRPG Combustion Conference, Aerospace Corp., El Segundo, Calif., 1965.
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