Karabeyoğlu, Mustafa ArifKara, Ozan2024-11-092021https://hdl.handle.net/20.500.14288/4163xix, 120 leaves. : tables ; 30 cm.restrictedAccessCarbon dioxideLiquid propellant rocketsRocket engines, CombustionAeronauticsPower resourcesIgnition capability of CO2 in hybrid rockets for mars ascent vehiclesDissertation© All Rights Reserved. Accessible to Koç University Affiliated Users Only!