Thermally Stable Burning Rate Accelerators

The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to...

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Bibliographische Detailangaben
Hauptverfasser:	Stephens, W D, Flanigan, D A, Hightower, J O, Miller, M, Willis, T C
Format:	Report
Sprache:	eng
Schlagworte:	ACETIC ACID ADDITIVES AERODYNAMIC CHARACTERISTICS ALUMINUM COMPOUNDS AMMONIUM PERCHLORATE ANHYDRIDES AROMATIC COMPOUNDS BALLISTIC MODIFIERS BURNING RATE CATALYSTS CHEMICAL MILLING CHLORIDES Combustion and Ignition CRYSTAL LATTICES FERROCENES FERROCENYL PROPELLANT INGREDIENTS FREEZE DRYING GRINDING GUIDED MISSILES HEAT SHIELDS HUMIDITY HYDROLYSIS INTERIOR BALLISTICS PARTICLE SIZE POLYMERS PURIFICATION RECRYSTALLIZATION (U) SOLID ROCKET PROPELLANTS REDUCTION ROCKET ENGINE CASES ROCKET MOTORS(SOLID PROPELLANT) SOLID ROCKET OXIDIZERS Solid Rocket Propellants SPRAY DRYING SPRAYS SUBLIMATION THERMAL INSULATION THERMAL STABILITY UFAPULTRAFINE AMMONIUM PERCHLORATE ULTRAFINES ULTRASONIC RADIATION
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Beschreibung
Zusammenfassung:	The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about -65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F.