Abstract: The invention provides a method for loading an application requiring personalization into a portable storage medium which is set up to be operated in a terminal. Personalization data for personalizing the application and possibly application data are additionally loaded into a restore module which is independent of applications stored in an application memory, is configured as a non-volatile memory, and is disposed within the portable storage medium or within the terminal. For updating an application, the personalization data and possibly application data are loaded from the restore module into the updated application. A portable storage medium has a non-volatile, application-independent restore module. System with storage medium and terminal and non-volatile, application-independent restore module.

Abstract: The invention provides a method for loading an application requiring personalization into a portable storage medium which is set up to be operated in a terminal. Personalization data for personalizing the application and possibly application data are additionally loaded into a restore module which is independent of applications stored in an application memory, is configured as a non-volatile memory, and is disposed within the portable storage medium or within the terminal. For updating an application, the personalization data and possibly application data are loaded from the restore module into the updated application. A portable storage medium has a non-volatile, application-independent restore module. System with storage medium and terminal and non-volatile, application-independent restore module.

Abstract: The present invention relates to double-base solid propellant mixtures whose burning characteristic is regulated by the addition of certain moderators such that the burn rates obtained are achieved independently of the temperature and pressure during the burn. This regulation is accomplished by the addition of a mixture of carbon black and cellulose acetate. The weight ratio of carbon black to cellulose acetate in this mixture is between 1:0.5 and 1:10. Depending on the composition of the solid propellant, the combustion of the rocket fuel can be regulated by regulating this mixture within the stated limits such that it takes place independently of temperature and pressure. The amount of the carbon black and cellulose acetate mixture present in the fuel can vary between 0.2 and 6% by weight; the carbon black is contained in the propellants of the invention in amounts between 0.05 and 1.0% by weight.