Master Thesis in Rocket Nutrition

Job ID: 36539161

Budget: $250 – $750 USD

Hello

I hope this message finds you well


I am seeking an expert in this subject
The topic is a Master's thesis in the art of rocket nutrition (liquid rockets), with a limit of 10,000 words, or 60 pages with a minimum of 80 references. The introduction should begin by defining the types of rockets, focusing on liquid rockets, and a specific system of rockets should be determined based on fuel, power, and size. I will then design the specific feeding system for this rocket system using a certain simulation program. There must be references available that provide details about the proposed feeding system so that the proposed system and its simulations can be designed.

Your task involves conducting a literature review to explore the current advancements in feed system design, specifically in relation to handling various propellants. In the event that extensive data and information are not readily available, you are encouraged to base your work on the available resources. The objective is to design feed systems for different propellants, including gaseous hydrogen, gaseous oxygen, and N2O.

Additionally, we have previously provided you with examples of such systems, such as Akash's thesis, which already have established requirements. We would like you to critically evaluate and challenge these examples, providing insights on potential improvements or alternative approaches to enhance their design and performance.


Kindly, contact me if you are an expert in this area and can handle the job well in a professional way.

Thanks