Results 91 to 100 of about 17,189 (237)
The Applications Technology Satellite apogee rocket motor - A summary report [PDF]
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applications Technology ...
Anderson, R. G.
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Electrical apparatus for detection of thermal decomposition of insulation Patent [PDF]
, 1971 Electrical failure detector in solid rocket propellant motor insulation against thermal degradation by fuel ...
Bernsen, B.
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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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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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Performance of rocket nozzle materials with several solid propellants [PDF]
Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid ...
Freche, J. C. +2 more
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Research on combustion instability and application to solid propellant rocket motors. II. [PDF]
, 1972 Unstable motions must be anticipated as a possible problem in solid-propellant rocket motors; the characteristics of an instability depend primarily on the geometry of the motor and composition of the propellant.
Culick, F. E. C.
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Particle size of aluminum oxide produced by a small rocket motor [PDF]
Spectrophotometric method for measurement of aluminum oxide particle sizes during burning of solid propellant rocket ...
Dobbins, R. A.
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Casting propellant in rocket engine [PDF]
, 1976 A method is described for casting a solid propellant in the casing of a rocket engine having a continuous wall with a single opening which is formed by leaves of a material which melt at a temperature of the propellant and with curved edges concentric to
Froehling, S. C., Roach, J. E.
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Solid rocket technology advancements for space tug and IUS applications [PDF]
In order for the shuttle tug or interim upper stage (IUS) to capture all the missions in the current mission model for the tug and the IUS, an auxiliary or kick stage, using a solid propellant rocket motor, is required.
Ascher, W. +3 more
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Design criteria monograph for pressurized metal cases [PDF]
, 1972 Organiation and presentation of data pertaining to design of solid propellant rocket engine cases are discussed. Design criteria are presented in form of monograph based on accumulated experience and knowledge.
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