A review of vaporization models as design criterion for bipropellant thrust chambers
MS Gontijo - Aerospace Technic and Technology, 2022 - nti.khai.edu
In the beginning of liquid propellant rocket engine development, the thrust chamber sizes
were obtained, mainly, empirically. With the technological advancements over the years …
were obtained, mainly, empirically. With the technological advancements over the years …