6
$\begingroup$

How does the trajectory vary between the two types of missions? Specifically, how does the speed and velocity vary for the booster for a Falcon 9 mission?

$\endgroup$
1
  • 5
    $\begingroup$ Check flightclub.io which has profiles for previous SpaceX flights (iirc the author corrects them by matching the telemetry data from webcast) together with estimated profiles for some upcoming missions. $\endgroup$
    – jkavalik
    Jul 18, 2016 at 12:42

1 Answer 1

-3
$\begingroup$

$Q2E \cdot \frac{VqE2}{Mass} \cdot \frac{thrust ratio}{V_e}$ on slow line exit to HEO to exit Ve to Max thrust to shut down and IqU2EvVe Is Pion Start up Pq2ExW/Mass to LqM x Ve = Tqr Thrust mass QVe to transition.

$\endgroup$
2
  • 5
    $\begingroup$ The site supports Latex formatting. I made a partial conversion of your formulas into latex, but I was incapable to decode, what you wanted to write. So if you know latex, please do the rest. Your formulas are probably incomprehensible for the readers in their current form. $\endgroup$
    – peterh
    Apr 2, 2018 at 5:23
  • 1
    $\begingroup$ how to write LaTeX/Mathjax: math.meta.stackexchange.com/questions/5020/… $\endgroup$
    – Hobbes
    Apr 2, 2018 at 7:11

Your Answer

By clicking “Post Your Answer”, you agree to our terms of service and acknowledge you have read our privacy policy.

Not the answer you're looking for? Browse other questions tagged or ask your own question.