Questions tagged [taylor-text]
Questions about the text "Introduction to Rocket Science and Engineering" by Travis S. Taylor
5
questions
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vote
1answer
81 views
I'm having a problem with the Throat Area formula derivation
I came upon this when reading "Introduction to Rocket Science and Engineering, he said "by differentiating" , my question is: differentiate with respect to what? and how do you get such ...
3
votes
1answer
477 views
Some exercise questions about Tsiolkovsky's Rocket Equation and Thrust Equation
I have found 6 of the question's answers, but I don't know they are correct. The last question about time of the burn I get negative result -0.42 seconds. Time could not be a negative value, so I ...
1
vote
1answer
751 views
Which components do we calculate for center of pressure? Where is the distance of components while computing the cp and cg of a rocket?
everybody!
I have 4 questions about center or pressure (cp) and center of gravity (cg) of a rocket system.
Questions
1) While computing the center of pressure of rocket system, which components do ...
3
votes
1answer
595 views
What are Mass Rate(∆v)/∆v, Mass Rate(Isp)/Isp and time of burn(MR)/MR graphs?
I have some problems about Tsiolkovsky's Rocket Equation and some graphs.
Firstly, I didn't get what I can do with Rocket Equation formulas as seen below,
Also, what these three graphs try to mean? ...
0
votes
1answer
549 views
Weight Flow Rate
I read in the book INTRODUCTION TO ROCKET SCIENCE AND ENGINEERING by T.S.T that Rocket Engineers design how big the throat of the nozzle should be based on the Weight Flow Rate.
So my question is HOW?
