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OERLIKON VERWALTUNGSGESELLSCHA
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OERLIKON VERWALTUNGSGESELLSCHA
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Application filed by OERLIKON VERWALTUNGSGESELLSCHAfiledCriticalOERLIKON VERWALTUNGSGESELLSCHA
Publication of ES261657A1publicationCriticalpatent/ES261657A1/es
Description of the m-1 high-performance rocket engine, using liquid oxygen and liquid hydrogen propellants, with a thrust rating of 1. 5 million pounds
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)