Hello! I am studying electronics engineering and since I always have an interest in rocketry, I deciced to correlate my interest with my graduation project.
I need to design a data acquisition system for a rocket which have the following specifications:
1-) Measuring a temperature value of a point located in the rocket that will reach 180 ⁰C in 120 ms.
2-) Measuring the pressure of the engine that provides necessary thrust for the rocket (Average temperature of the engine is anticipated to be 1800 ⁰K)
I need to transmit these values to a ground control station. First step is selecting the sensors, components that will operate in conditions mentioned above
and drawing the block diagram of the system. As I tried to search components on the internet, I couldn't find sensors that operates in these extreme conditions.
Can someone guide me about how to proceed and what to consider designing such a system?
Thanks in advance.
I need to design a data acquisition system for a rocket which have the following specifications:
1-) Measuring a temperature value of a point located in the rocket that will reach 180 ⁰C in 120 ms.
2-) Measuring the pressure of the engine that provides necessary thrust for the rocket (Average temperature of the engine is anticipated to be 1800 ⁰K)
I need to transmit these values to a ground control station. First step is selecting the sensors, components that will operate in conditions mentioned above
and drawing the block diagram of the system. As I tried to search components on the internet, I couldn't find sensors that operates in these extreme conditions.
Can someone guide me about how to proceed and what to consider designing such a system?
Thanks in advance.