Reference Books

  • George P. Sutton, Oscar Biblarz: Rocket Propulsion Elements
  • John R. London: LEO on the Cheap
  • Gerald K. O'Neil: The High Frontier

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August 26, 2009

Comments

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john hare

I would say the 5 segment is about the same as the 4 segment, both EE. My computer didn't access the calculator for some reason, probably operator error.

John Bossard

John, my friend, there's no need to guess at the answer, that's what the calculator's for!
For the 5-segment SRB, try using 3,600,000 lbf of thrust and a burn time of 120 seconds.
I'll email you the .xls file.

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