X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=rockets%2Fresearch%2F2017-test-05.mdwn;h=232ff56e767dd6aff29098291fdacba02acc1632;hb=2297feecab2d9ee0b9ca01f246aef2dc4da7592e;hp=250f080868a86bf6b9ac2486f04a6ff1f06f48a3;hpb=f8a923245d05b3f8f2e12b39e7a28253aaea26fe;p=web%2Fgag.com diff --git a/rockets/research/2017-test-05.mdwn b/rockets/research/2017-test-05.mdwn index 250f080..232ff56 100755 --- a/rockets/research/2017-test-05.mdwn +++ b/rockets/research/2017-test-05.mdwn @@ -3,12 +3,18 @@ 3 grain 54mm sorbitol motor With a 10.250" liner, 8.9mm nozzle throat, buna-n o-rings, simulation says -this is a 25% J-432, 763 Ns, with about a 1.6 sec burn +this is a 25% J-432, 763 Ns, with about a 1.6 sec burn: + + +
54mm 3-grain Sorbitol | |||||
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Rating: | 25% J-432 | Max Pressure: | 7.04 MPa (1021 psi) | ||
Total Impulse: | 763 Ns | Specific Impulse: | 135 s | ||
Max Thrust: | 557 N | Volume Loading: | 71% | ||
Average Thrust: | 432 N | Fuel Mass: | 578 g | ||