ROCKET PERMITTING COMBUSTION CONTROL AND SPEED CONTROL AND BEING CHARGED WITH SOLID FUEL IN KNEADED FORM

摘要

PURPOSE:To permit the restriction of combustion and speed control by using the solid fuel in semi-kneaded form as the fuel charged into the inside tank of a rocket. CONSTITUTION:The inside tank 2 of a rocket 1 is filled with the solid fuel 8 in semi-kneaded form. In flight, the solid fuel 8 in semi-kneaded form is supplied into a combustion chamber 6 through an adjusting valve 4 by a fuel pump 3, and the high pressure gas generated after the combustion in the combustion chamber 6 is jetted out from a nozzle 7, and a thrust force is obtained. Therefore, combustion control and speed control are facilitated by controlling the quantity of supply of the solid fuel in semi-kneaded form by the adjusting valve 4.