Results 81 to 90 of about 9,342 (197)
Effects of Ionizing Radiation on Solid Rocket Motor Components [PDF]
, 1961 Problems which the solid propellant rocket engineer will encounter in designing for long-term storage in a radiation environment are discussed. A summary of present knowledge of the radiation environment is given.
Gardner, Richard E.
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Study of vortex valve for medium temperature solid propellants [PDF]
, 1966 Fluid state vortex valve secondary injection control system shows considerable promise for future application to solid propellant rocket engine thrust vector control.
Holt, W. D., Rivard, J. G.
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Hydrogen/oxygen auxiliary propulsion technology [PDF]
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thrust H/O rocket technology. A review of H/O APS studies performed for the Space Shuttle, Space Tug, Space Station Freedom, and Advanced Manned Launch ...
Reed, Brian D., Schneider, Steven J.
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Storage of solid propellants in a dry environment [PDF]
Storage of solid propellants in either a dry or a vacuum environment causes a significantly greater increase in the propellants' modulus and maximum tensile strength than does ambient storage.
Udlock, D. E.
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Inhibited solid propellant composition containing beryllium hydride [PDF]
, 1978 An object of this invention is to provide a composition of beryllium hydride and carboxy-terminated polybutadiene which is stable. Another object of this invention is to provide a method for inhibiting the reactivity of beryllium hydride toward carboxy ...
Thompson, W. W.
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The University of Arizona program in solid propellants [PDF]
The University of Arizona program is aimed at introducing scientific rigor to the predictability and quality assurance of composite solid propellants. Two separate approaches are followed: to use the modern analytical techniques to experimentally study ...
Ramohalli, Kumar
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A study of the application of microwave techniques to the measurement of solid propellant burning rates Progress report, 1 Sep. 1966 - 31 Aug. 1967 [PDF]
Microwave techniques for measurement of solid rocket propellant burning ...
Obrien, W. F., Jr., Wood, H. L.
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Composite engines for application to a single-stage-to-orbit vehicle [PDF]
Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine.
Bendot, J. G. +2 more
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Solid rocket motor internal insulation [PDF]
Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant.
Keller, R. B., Jr., Twichell, S. E.
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Orbital Maneuvering system design evolution [PDF]
, 1985 Preliminary design considerations and changes made in the baseline space shuttle orbital maneuvering system (OMS) to reduce cost and weight are detailed.
Gibson, C., Humphries, C.
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