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Dynamit Nobel AG
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Dynamit Nobel AG
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Priority to ES339805ApriorityCriticalpatent/ES339805A1/es
Publication of ES339805A1publicationCriticalpatent/ES339805A1/es
Mécanisme d'amenée pour un dispositif de lancement de missiles téléguidés à propulsion par réaction, destiné en particulier à des véhicules blindés
The effects of solid propellant rocket exhaust on elastomeric protective coatings(Erosion resistance tests of elastomeric protective coatings under solid propellant motor firing)
Device for instantaneous supply or cutoff of a fuel component in a liquid-propellant rocket engine(Device for instantaneous supply or cutoff of fuel component in liquid propellant rocket engine)
Preliminary report on the performance of plug nozzles in solid propellant rockets(Test program for data on plug nozzle behavior especially for solid propellant rockets, noting similarity with de Laval type nozzles)
Use of gasdynamic thrust vector control with solid propellant rocket engines, involving the secondary injection of mass into the main supersonic rocket jet
A propellant depletion system for propulsion shut-down on the atlas space launch vehicle(Liquid propellant depletion system for propulsion shutdown on atlas centaur launch vehicle)
A scintillation detection system for the inspection of large solid propellant rocket motors(Scintillation detection for the inspection of large solid propellant rocket motors)