Ignition catalysts for furfuryl alcohol - Red fuming nitric acid bipropellant

Abstract

References 1 Alien, H. J. and Eggers, A. J., A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth Atmosphere at High Supersonic Speeds, Rept. 1381, 1958, NACA. 2 Leon, H. I., Angle of Attack Convergence of a Spinning Missile Descending Through the Atmosphere, Journal of the Aerospace Sciences, Vol. 25, No. 8, 1958, pp. 480-484. 3 Garber, T. B., On the Rotational Motion of a Body ReEntering the Atmosphere, Journal of the Aerospace Sciences, Vol. 26, No. 7, 1959, pp. 443-449. 4 Coakley, T. J., Stability of Symmetric Spinning Missiles, AIAA Journal, Vol. 5, No. 10, Oct. 1968, pp. 12311232. 5 Jaffe, P., Terminal Dynamics of Atmospheric Entry Capsules, AIAA Journal, Vol. 7, No. 6, June 1969, pp. 11571158. 6 Nayfeh, A. H., A Multiple Time Scaling Analysis of Reentry Body Roll Dynamics, Transactions of the Third Technical Workshop on Dynamic Stability Problems, NASA Ames Research Center, Nov. 1968; also AIAA Journal, Vol. 7, No. 11, Nov. 1969, pp.2155-2157. 7 Flatus, D. H., Angle-of-Attack Convergence and WindwardMeridian Rotation Rate of Rolling Re-Entry Vehicles, Transactions of the Third Technical Workshop on Dynamic Stability Problems, NASA Ames Research Center, Nov. 1968; also AIAA Journal, Vol. 7, No. 12, Dec. 1969, pp. 2324-2330. 8 Equilibrium Roll Rate Theory for a Re-entry Vehicle, Document 67SD234, 1967, General Electric Co.