Development of low cost ablative nozzles for solid propellant rocket motors, volume 1 Final report [PDF]
Evaluating low cost ablative materials for use in large solid propellant rocket ...
Laramee, R. C., Mathis, J. R.
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Investigation of the rocket motor dimensionless geometric parameters influence on the burning rate of double base propellant [PDF]
, 2001 Lajoš Tot, Panto Maslak
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On a problem of thermo-viscoelasticity [PDF]
Analysis of viscoelastic materials under transient thermal conditions related to solid rocket ...
Knauss, W. G., Pucik, P. A.
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CSM programs SM RCS propellant quantity gaging systems program [PDF]
, 1971 Computer program calculates actual and useable remaining propellant quantities as required in positive expulsion rocket engine propellant feed system. Program establishes relationship between helium system pressures and temperatures and propellant weight
Cox, G. R., Reynolds, R. G.
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On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]
, 2001 С. А. Шевченко
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Nonlinear combustion instability in liquid-propellant rocket motors Final report [PDF]
Mathematical models of nonlinear combustion instabilities in liquid propellant rocket ...
Burstein, S. Z. +2 more
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Case Study of Combustion Instability in Solid Propellant Rocket Motors [PDF]
, 2003 Myeong-Won Yun, Gyeong-Mu Kim
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Second 260-Inch Solid Motor Set for Test Firing [PDF]
Second 260-inch diameter solid propellant rocket engine set for test ...
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Propellant-powered actuator for gas generators [PDF]
, 1972 Hydrazine operated monopropellant generators are used for spacecraft rocket engines and propellant pressurization systems.
Makowski, M. J.
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The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
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