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2 votes
0 answers
152 views

Rocket Launch Azimuth Calculation

EDIT 2: I was told immediately when I explained this problem in other places that a closed loop guidance system would be necessary. I knew this was the case from the start and moreso, when I realized ...
rymach's user avatar
  • 21
1 vote
0 answers
112 views

How high will this rocket be, when MECO occurs?

Find the altitude of the rocket at the time of engine cut-off. Rocket Mass = 369208 kg, Rocket Area = 391 m2, Fuel = 170697 L, Fuel density = 21 kg/l, Exhaust Speed = 1338 m/s, Exhaust Area = 164 m2
Praveen Kumar's user avatar
3 votes
1 answer
154 views

What is missing in the conversion of specific impulse from units of seconds to thrust/mass flow rate? [duplicate]

I was trying to get the Specific Impulse of the Saturn V engines, hoping for a value in N/kg/s, as I need to know the mass consumption rate per thrust value. Any and all sources give me the value in ...
confused_aspirant's user avatar
1 vote
0 answers
71 views

What is the best place on the internet to learn basic physics needed for rocket engineering? [closed]

Does anyone know a site where everything is in one place and it teaches equations and pricipals from the basics?
Filip's user avatar
  • 11
6 votes
2 answers
787 views

Modeling a rocket using Tsiolkovsky's equation and ordinary differential equations

So I have this uni assignment to make a model out of ODEs, and my idea was to use rockets. After some research I found about Tsiolkovsky's equation and tried using it on a Falcon 9 (disconsidering ...
Yodaperor's user avatar
3 votes
5 answers
988 views

Why is hydrogen better than helium as remass?

I just watched a very good YouTube video on why nuclear engines might be useful, and it also goes into why Hall Effect thrusters are super good at squeezing obscene ISP out of things. During the video,...
William Walker III's user avatar
3 votes
1 answer
478 views

Pendulum rocket fallacy - so why *do* skyrockets have sticks?

This question is inspired by two, linked questions. Skyrockets (of the pyrotechnic/firework kind) have guide sticks, which are (according to internet sources) to enhance stability: "The guide ...
abligh's user avatar
  • 131
20 votes
4 answers
8k views

What is the "pendulum rocket fallacy" as it relates to analogizing a pencil balanced on a finger to maintaining attitude of a hovering rocket?

I've received comments that explain to me that the analogy between rocket attitude control during a hovering maneuver and the act of balancing pencil on the end of a finger is a helpful and good one; ...
uhoh's user avatar
  • 148k
4 votes
2 answers
756 views

Design of starship fins

How much can the falling speed of starship approximately be reduced by the bellyflop fall with fins? Are we talking about numbers around 5% or 50% here? Wouldn't it make sense to put holes where the ...
fipps omat's user avatar
5 votes
1 answer
799 views

Contracting rocket engine nozzles

The efficiency of rocket engine nozzles depends greatly on their expansion ratio an how well the ambient pressure matches the rocket nozzles exit pressure. An optimal expansion ratio means that there ...
publicdomain's user avatar
  • 1,222
1 vote
0 answers
436 views

Can Chemical Engineer work on something related to space?

I am an undergraduate student (scientific section) living in Qatar. I have a big interest in astronomy and astrophysics and have participated in the IOAA (International Olympiad on Astronomy and ...
sara nabil's user avatar
4 votes
3 answers
3k views

What (if anything) limits the efficiency of a rocket engine?

Humans have developed lots of rockets. I observe that in most cases to increase the payload capacity we just increase the amount of fuel. Is it not possible to exponentially increase the efficiency ...
Akshat's user avatar
  • 79
13 votes
6 answers
3k views

Why does this formula say rocket efficiency depends on velocity?

Wikipedia gives the following equation for the efficiency $\eta_p$ of an engine here: $$\eta_p= \frac {2\, (\frac {v} {v_e})} {1 + ( \frac {v} {v_e} )^2 }$$ where $v$ is the rocket speed and $v_e$ ...
Nightrider's user avatar
  • 2,035
9 votes
5 answers
5k views

Why do space rockets not start from an angle? Why go straight up? [duplicate]

I know that they used to have this idea, back in the day, of a "space gun" to fire somebody into space, and I understand why that was not safe or practical/feasible. However, once they had come up ...
Bidal's user avatar
  • 107
2 votes
1 answer
2k views

How did NASA calculate 22 million "rocket horsepower" for the SLS Booster?

This answer to Does NASA really report the power of rockets in horsepower? cites NASA news item Space Launch System Booster Aimed and Ready to Fire which says "What's impressive about this test is ...
uhoh's user avatar
  • 148k

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