X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=rockets%2Fresearch%2F2017-test-12.mdwn;h=ba35937b2a8ca188c6a2447bb508b3dd7294d3c2;hb=2297feecab2d9ee0b9ca01f246aef2dc4da7592e;hp=81f314f18a6e8fb525b1a1372c2888895686c12e;hpb=3e16c14fa8347986b349ee98b7705a5ab6368e85;p=web%2Fgag.com diff --git a/rockets/research/2017-test-12.mdwn b/rockets/research/2017-test-12.mdwn index 81f314f..ba35937 100755 --- a/rockets/research/2017-test-12.mdwn +++ b/rockets/research/2017-test-12.mdwn @@ -9,24 +9,32 @@ ring plus 0.25" inside liner, with two o-rings, one pushing against liner. Liner 23.125" long with about 22.25" available for fuel load. -Had to trim grains to fit. Four just required squaring up the ends and -trimming excess casting tube away. Fifth one was cut in miter box with saw. +Simulation says this is a 57% L-1366 with 3804 Ns total impulse, 797 psi max, +76% volume loading, and about 2.6 seconds burn time. -O-rings made forward closure a *very* snug fit. + +
CTI mod Sorbitol | |||||
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Rating: | 57% L-1366 | Max Pressure: | 5.5 MPa | ||
Total Impulse: | 3804 Ns | Specific Impulse: | 131 s | ||
Max Thrust: | 1706 N | Volume Loading: | 76% | ||
Average Thrust: | 1366 N | Fuel Mass: | 2958 g | ||