X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_G75_1.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_G75_1.eng;h=e3e4aa5df664c118fe3f7c22fee941b7819782ae;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_G75_1.eng b/datafiles/thrustcurves/AeroTech_G75_1.eng new file mode 100644 index 00000000..e3e4aa5d --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_G75_1.eng @@ -0,0 +1,83 @@ +; +; Aerotech G75J (Black Jack) +; +; AeroTech RMS-29/180 Easy Access Reloadable Motor Hardware. +; +; RASP.ENG file made from made from NAR or TMT published data. +; +; File produced May, 17 2004. +; +; The total impulse, peak thrust, average thrust and burn time are +; the same as the averaged static test data from NAR or TMT files. +; +; The curve drawn with these data points is as accurate as could +; could be made scaling the data from the curve on the TMT html +; page. The file is 63 data points. NOT wRASP v1.6 compatible. +; +; The file was created by Stan Hemphill. +; Contact at stanley_hemphill@hotmail.com. +; +; Motor Dia Len Delay Prop Gross Mfg +G75J 29 194 1-3--4-6-7-9-10 0.114 0.236 AT +0.0281 068.8604 +0.0380 078.6517 +0.0561 075.9230 +0.0660 073.0337 +0.0776 070.4655 +0.1139 069.3419 +0.1403 068.6998 +0.1667 067.5762 +0.1881 070.3050 +0.2013 069.0209 +0.2294 072.5522 +0.2541 076.4045 +0.2723 071.4286 +0.3102 076.2440 +0.3350 071.9101 +0.4208 075.6019 +0.4604 072.3917 +0.5215 079.2937 +0.5941 073.3547 +0.6436 080.0963 +0.7013 073.8363 +0.7393 076.4045 +0.7541 074.6388 +0.7657 077.3676 +0.7937 078.6517 +0.8036 077.0465 +0.8168 080.2568 +0.8267 075.2809 +0.8383 081.5409 +0.8581 075.7624 +0.8795 077.8491 +0.9340 074.1573 +0.9868 079.9358 +1.0380 076.7255 +1.0561 072.2311 +1.0941 078.8122 +1.1221 075.6019 +1.1502 080.8989 +1.1617 076.8860 +1.1848 080.0963 +1.1997 076.7255 +1.2327 078.8122 +1.2508 076.4045 +1.2871 082.5040 +1.3102 077.5281 +1.3267 081.8620 +1.3564 075.2809 +1.3729 080.0963 +1.4076 075.7624 +1.4884 079.9358 +1.5116 073.6758 +1.5297 081.0594 +1.5512 074.6388 +1.5611 080.8989 +1.6040 072.8732 +1.7211 075.6019 +1.7607 068.6998 +1.7789 070.1445 +1.8119 066.9342 +1.8267 070.7865 +1.8482 070.7865 +2.3878 000.0000