Browsing by Author "Hamzah Alghadeer, Noor"
Now showing 1 - 1 of 1
Results Per Page
Sort Options
Item MULTISTAGE LAUNCH VEHICLE DESIGN(2022-02-15) Hamzah Alghadeer, Noor; Inger, ErkIn this thesis, we designed a multistage launch vehicle. In the first stage, it uses a liquid propellant in a booster with five solid rocket propellants to reach about 42 km. In the second stage, after rejecting the five solid rocket propellants to reduce the weight and used liquid propellant only to reach the low earth orbit (LEO) at 925 Km altitude in order to transfer satellite for science study. After finishing the design, three case studies for this design. The first case studied the effect of a number of solid rockets with a velocity of the rocket. A second case study is dealing with an altitude of the rocket and the number of the solid rocket. The last case was dealing with an altitude of the rocket and the orbit velocity at the same altitude.