ES246249A1 - Intensive ignition rocking motor with rear and reverse front nozzles. (Machine-translation by Google Translate, not legally binding)
- Google Patents
Intensive ignition rocking motor with rear and reverse front nozzles. (Machine-translation by Google Translate, not legally binding)
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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RODRIGUEZ VILLA ANDRES
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RODRIGUEZ VILLA ANDRES
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Priority to ES0246249ApriorityCriticalpatent/ES246249A1/en
Publication of ES246249A1publicationCriticalpatent/ES246249A1/en
Pharmaceuticals Containing Other Organic And Inorganic Compounds
(AREA)
Abstract
Intensive ignition rocket engine with rear and front reversion nozzles, essentially characterized by the propellant gases produced by a solid load that develops a high thrust force and has a short reaction time, thus allowing the use of very long grains without deformation of them by pressure. Simultaneously by the tail and front of the motor through one or several nozzles. (Machine-translation by Google Translate, not legally binding)
ES0246249A1958-12-271958-12-27Intensive ignition rocking motor with rear and reverse front nozzles. (Machine-translation by Google Translate, not legally binding)
ExpiredES246249A1
(en)
The application of numerical methods to the solution of structural integrity problems of solid propellant rockets(High speed digital computer methods in solution of structural dynamics problems for solid propellant rocket engines and stress analysis and listing of computer programs)