Development of a Hybrid Rocket Slab Motor
R Theba, KL Veale, C Bemont - 52nd AIAA/SAE/ASEE Joint Propulsion …, 2016 - arc.aiaa.org
R Theba, KL Veale, C Bemont
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016•arc.aiaa.org𝐴𝑖𝑛𝑗= area of injector 𝐴𝑝= area of the port 𝑎= regression rate coefficient/ballistic
coefficient 𝐶𝑑= coefficient of discharge 𝐺𝑜𝑥= oxidizer mass flux 𝑚̇𝑜𝑥= oxidizer mass flow
rate 𝑚̇𝑓= fuel mass flow rate 𝑁𝑖𝑛𝑗= number of injector holes 𝑛= mass flux
exponent/ballistic coefficient 𝑂 𝐹⁄= oxidizer-to-fuel ratio∆ 𝑃= pressure drop 𝜌𝑜𝑥= oxidizer
density
coefficient 𝐶𝑑= coefficient of discharge 𝐺𝑜𝑥= oxidizer mass flux 𝑚̇𝑜𝑥= oxidizer mass flow
rate 𝑚̇𝑓= fuel mass flow rate 𝑁𝑖𝑛𝑗= number of injector holes 𝑛= mass flux
exponent/ballistic coefficient 𝑂 𝐹⁄= oxidizer-to-fuel ratio∆ 𝑃= pressure drop 𝜌𝑜𝑥= oxidizer
density
𝐴𝑖𝑛𝑗= area of injector 𝐴𝑝= area of the port 𝑎= regression rate coefficient/ballistic coefficient 𝐶𝑑= coefficient of discharge 𝐺𝑜𝑥= oxidizer mass flux 𝑚̇𝑜𝑥= oxidizer mass flow rate 𝑚̇𝑓= fuel mass flow rate 𝑁𝑖𝑛𝑗= number of injector holes 𝑛= mass flux exponent/ballistic coefficient 𝑂 𝐹⁄= oxidizer-to-fuel ratio∆ 𝑃= pressure drop 𝜌𝑜𝑥= oxidizer density
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