Compilation of rocket spin data. Volume 2 - Literature survey Final report, Nov. 1966 - Aug. 1968 [PDF]
Literature survey of acceleration spin effects on solid propellant rocket ...
Manda, L. J.
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Combustion chemistry of solid propellants [PDF]
Several studies are described of the chemistry of solid propellant combustion which employed a fast-scanning optical spectrometer. Expanded abstracts are presented for four of the studies which were previously reported.
Baer, A. D., Ryan, N. W.
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Modifying burning rate and agglomeration size in aluminized composite solid propellants using mechanically activated metals [PDF]
Agglomeration reduction techniques are important field in solid propellant industry, Large agglomeration results in excessive two phase losses. Tailored composite particles has been applied to tailor aluminum particle ignition and combustion.
Belal, Hatem Mohamed
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Tactical Missile Performance for Single and Multi-Wire Embedded Propellant Configurations with Discontinuities [PDF]
This research analyzes the performance of a nominal air-to-air tactical missile with varying configurations of wire-embedded end-burning solid propellant grains.
Wilson, Paul B.
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Design of a test bench for solid rocket motors and complete flight rocket vehicles [PDF]
In this report an extensive explanation of the Final Degreeās Thesis Design of a test bench for solid rocket motors and complete flight rocket vehicles can be found.
Tortosa Masbernat, Ernest
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innovative solid formulations for rocket propulsion [PDF]
Solid rocket propulsion enjoys several unique properties favoring its use in space exploration and military missions still for decades to come, in spite of being by far the most mature propulsion technology among those currently employed.
L. T. DeLuca
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Structure and property of propellant based on nitroglycerine/glycerol triacetate mixed plasticizers: molecular dynamics simulation and experimental study. [PDF]
Yang L, Wu X, Li J, Chen T, Liu M, He Q.
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Research progress of EMOFs-based burning rate catalysts for solid propellants. [PDF]
Tan B +5 more
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Fabrication of CL-20/HMX Cocrystal@Melamine-Formaldehyde Resin Core-Shell Composites Featuring Enhanced Thermal and Safety Performance via In Situ Polymerization. [PDF]
Duan B +5 more
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Manufacture and static firing of X259-E6 rocket motor serial number XJ04/0001 [PDF]
A single motor was cast and static fired to demonstrate the performance of high energy crosslinked double base (XLDB) propellant in standard X259 rocket motor hardware.
Robertson, D. R.
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