Results 181 to 190 of about 7,227 (196)

Ignition transient control through inhibiting of propellant grain

Solid Propellant Rocket Conference, 1964
THHERE is a real need in the solid propellant industry for JL a simple, inexpensive means of controlling the ignition transient performance of a rocket motor. Too frequently the rate of pressure rise and/or the peak pressure of a new motor are excessive causing serious, expensive, and time-consuming delays.
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The Strain Analysis of Solid Propellant Rocket Grains

Journal of the Aerospace Sciences, 1960
There is often a wide divergence of interest between the missile engineer responsible for thrust performance on the one hand, and the motor tube manufacturer concerned with chemical composition on the other. The propellant grain design analj^st interested in structural integrity is, therefore, frequently hard put to compromise both aims efficiently in ...
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NUMERICAL ANALYSIS OF GRAIN BURNBACK IN SOLID PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion, 2002
COLASURDO, GUIDO, CASALINO, LORENZO, PASTRONE, Dario Giuseppe, L. PIANTINO   +3 more
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MATHEMATICAL MODEL FOR PROPELLANT GRAIN GEOMETRY REGRESSION

Procceedings of the 19th Brazilian Congress of Thermal Sciences and Engineering, 2022
Leib Neubarth, Rachel Manhães de Lucena, Norberto Mangiavacchi, Daniel Chalhub, GIL ROBERTO VIEIRA. PINHEIRO, José da Rocha Miranda Pontes, Maurício Ferrapontoff Lemos, LAURILIO SILVA JUNIOR   +7 more
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EXTRUSION TECHNIQUE FOR EXTRUDED COMPOSITE PROPELLANT GRAIN

International Journal of Energetic Materials and Chemical Propulsion, 2016
Ashwani K. Mishra, A. N. Patil, A. B. Dange, R. N. Patkar, P. K. Khanna, Seema D. Kakade   +5 more
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Additive Manufacturing of Solid Rocket Propellant Grains

Journal of Propulsion and Power, 2018
Chandru, RA, Balasubramanian, Nikhil, Oommen, Charlie, Raghunandan, BN   +3 more
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REMOVED: Solid Propellant Grain Design

1993
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Thermal stresses in a finite solid-propellant grain

2014
In order to gain a fundamental understanding of actual solid propellant thermal stress problems, the geometry of the solid propellant baa been idealized as a short, circular cylinder with flat ends. It is felt that the consideration of actual curved ends would only unduly have complicated the analysis. The method of solution for the thermal stresses in
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Solid-propellant grain-to-mandrel adhesion phenomena

Journal of Spacecraft and Rockets, 1970
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REMOVED: Structural Analysis of Propellant Grains

1993
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