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General Info and data files for comparison #46

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@benrussell11

Hi Andrew,

I posted the following on the Rocketry Forum and have moved it to here. Hopefully that is ok.

I haven't used GitHub before, so bear with me. How do I set the issue type?

I've put together Zip file which contains my IREC team's characterization testing. A couple of notes:

  • ProPEP 3 was used to determine propellant characterics - A&N etc.
  • Their goal is a 98 mm 10 - 20 % N with a smoke grain.

The zip file contains the following:

    1. *.txt - static test data. File name is the throat in 64's
    1. *.bsx - Burnsim files - Propellant is 2019 IREC Blue
    1. *.ric - openMotor files - Propellant is 2019 IREC Blue
    1. 76mm Characterization Tests.xlsx - Test data. Average and Maximum Pressure calculated and burn time.
    1. 98 2nd Static Test.bsx - Burnsim for next static test
    1. 98 2nd Static Test.ric - openMotor for next static test
    1. 98 2nd Static Test with smoke grain.bsx - Takes into account the 1" propellant delay grain
    1. 98 2nd Static Test with smoke grain.ric - Takes into account the 1" propellant delay grain
    1. 2019 IREC Test data.MTD2 - ProPEP3 - average pressure is used calculate A&N

General notes for the above

  • For the static test burns, openMotor and Burnsim are close and compare well to the test data.
  • However, they do differ in the total impulse and calculated thrust/force.
  • Since I used average pressure to calculate A&N etc, Burnsim and openMotor max pressure matches the average pressure. Curious, do you use max or average pressure to calculate A&N?
  • I believe this motor is a little on the erosive side.

IREC Test Data.zip

Ben

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