Ogival System
The vaulting framework of intersecting pointed arch ribs
Ogival system is a type of rocket propulsion system that uses solid propellant to generate thrust. This system is named after its inventor, French engineer and inventor Claude G. Ogive. The ogival system is a type of solid rocket engine, which means that the fuel and oxidizer are mixed together in a solid block rather than being stored separately.
The ogival system works by igniting the solid propellant, which then burns in a controlled manner to generate a high-velocity exhaust stream. This exhaust stream produces the thrust required to propel the rocket forward. The outer casing or nozzle of the rocket is designed to shape and direct the exhaust stream for maximum efficiency.
One of the advantages of the ogival system is its relative simplicity and reliability compared to other types of rocket engines. Because the fuel is already mixed and solidified, there is no need for complex plumbing or pumps to deliver it to the combustion chamber. This makes the ogival system more resistant to malfunctions caused by leaks or other failures in the fuel delivery system.
Another advantage of the ogival system is its ability to produce high thrust for a relatively low cost. Because the solid propellant is inexpensive and widely available, ogival engines are often used in low-cost rockets and missiles.
Overall, the ogival system is a useful and reliable rocket propulsion technology that has been used in a wide range of applications, from military missiles to space launch vehicles.
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