摘要:
In order to make a drive device available on the basis of a gel-type propellant, in particular, for a flying object, comprising at least one tank for gel-type propellant, a combustion chamber and a device for supplying propellant to the combustion chamber, which is of a simple construction it is suggested that at least one radiation impinging device be provided for acting on gel-type propellant with electromagnetic radiation and/or at least one heating device for heating gel-type propellant in order to improve the flow behavior.
摘要:
So as to create a combustion chamber, especially for a rocket propulsion unit, comprising a combustion chamber, an inner casing surrounding said combustion chamber, an outer casing surrounding the inner casing and coolant channels embodied between the inner and outer casing, the casing of which has improved thermal resistance and a greater mechanical load-bearing capacity, the invention provides for the outer casing to be made of a fibro-ceramic material and for the inner casing to made of a fibro-ceramic material or graphite.