version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_F21.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="189.81" Itot="55.842" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.202" burn-time="2.52" cgDiv="10" cgFix="1" cgStep="-1." code="F21W" delays="4,6,8" dia="24." exitDia="0." initWt="64." len="96." mDiv="10" mFix="1" mStep="-1." massFrac="46.88" mfg="Aerotech" peakThrust="42.504" propWt="30." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>Aerotech F21W (White Lightning) RASP.ENG file.\r
5 File produced Jun 22 2004.\r
6 The file was produced by scaling data points off the\r
7 thrust curve in the Tripoli.org motor pdf file.\r
8 \r
9 The F21W cannot be found on thrustcurve.org.\r
10 Hence the amateur file production.\r
11 The file was created by Stan Hemphill\r
12 Contact at stanley_hemphill@hotmail.com;\r
13 </comments>\r
14 <data>\r
15 <eng-data cg="48." f="0." m="30." t="0."/>\r
16 <eng-data cg="48." f="37.2266" m="29.955" t="0.0045"/>\r
17 <eng-data cg="48." f="42.1474" m="29.8591" t="0.009"/>\r
18 <eng-data cg="48." f="42.504" m="29.6544" t="0.018"/>\r
19 <eng-data cg="48." f="40.5071" m="29.4537" t="0.027"/>\r
20 <eng-data cg="48." f="38.8669" m="29.3109" t="0.0337"/>\r
21 <eng-data cg="48." f="38.225" m="29.1245" t="0.0427"/>\r
22 <eng-data cg="48." f="37.7258" m="28.9409" t="0.0517"/>\r
23 <eng-data cg="48." f="36.87" m="28.7606" t="0.0607"/>\r
24 <eng-data cg="48." f="36.4422" m="28.538" t="0.072"/>\r
25 <eng-data cg="48." f="36.4422" m="28.2307" t="0.0877"/>\r
26 <eng-data cg="48." f="35.3724" m="27.7966" t="0.1102"/>\r
27 <eng-data cg="48." f="35.8716" m="27.322" t="0.135"/>\r
28 <eng-data cg="48." f="35.4437" m="26.9351" t="0.1552"/>\r
29 <eng-data cg="48." f="36.2282" m="26.5885" t="0.1732"/>\r
30 <eng-data cg="48." f="35.6577" m="26.0228" t="0.2025"/>\r
31 <eng-data cg="48." f="37.2979" m="25.186" t="0.2452"/>\r
32 <eng-data cg="48." f="36.5848" m="24.4259" t="0.2835"/>\r
33 <eng-data cg="48." f="38.0111" m="23.7045" t="0.3195"/>\r
34 <eng-data cg="48." f="37.4406" m="23.3397" t="0.3375"/>\r
35 <eng-data cg="48." f="38.5816" m="22.5596" t="0.3757"/>\r
36 <eng-data cg="48." f="38.225" m="22.1408" t="0.396"/>\r
37 <eng-data cg="48." f="39.3661" m="21.4384" t="0.4297"/>\r
38 <eng-data cg="48." f="38.0111" m="21.1121" t="0.4454"/>\r
39 <eng-data cg="48." f="38.7242" m="20.5082" t="0.4747"/>\r
40 <eng-data cg="48." f="37.7971" m="20.2307" t="0.4882"/>\r
41 <eng-data cg="48." f="38.1537" m="19.8186" t="0.5084"/>\r
42 <eng-data cg="48." f="38.5103" m="19.2626" t="0.5354"/>\r
43 <eng-data cg="48." f="37.9398" m="18.6609" t="0.5647"/>\r
44 <eng-data cg="48." f="37.2266" m="18.253" t="0.5849"/>\r
45 <eng-data cg="48." f="37.8685" m="17.9343" t="0.6007"/>\r
46 <eng-data cg="48." f="36.87" m="17.1674" t="0.6389"/>\r
47 <eng-data cg="48." f="37.1553" m="16.5411" t="0.6704"/>\r
48 <eng-data cg="48." f="35.9429" m="14.6856" t="0.7649"/>\r
49 <eng-data cg="48." f="32.9477" m="11.8136" t="0.9201"/>\r
50 <eng-data cg="48." f="30.309" m="10.3608" t="1.0056"/>\r
51 <eng-data cg="48." f="29.7385" m="9.30753" t="1.0709"/>\r
52 <eng-data cg="48." f="24.0333" m="6.51409" t="1.2643"/>\r
53 <eng-data cg="48." f="24.0333" m="6.22359" t="1.2868"/>\r
54 <eng-data cg="48." f="20.8241" m="5.19337" t="1.3723"/>\r
55 <eng-data cg="48." f="20.8241" m="4.96627" t="1.3926"/>\r
56 <eng-data cg="48." f="15.4754" m="3.05808" t="1.5883"/>\r
57 <eng-data cg="48." f="15.4754" m="2.87102" t="1.6108"/>\r
58 <eng-data cg="48." f="5.0634" m="0.662014" t="2.0112"/>\r
59 <eng-data cg="48." f="3.4231" m="0.415818" t="2.1192"/>\r
60 <eng-data cg="48." f="2.4247" m="0.224965" t="2.2407"/>\r
61 <eng-data cg="48." f="1.4976" m="0.0803083" t="2.378"/>\r
62 <eng-data cg="48." f="0.9271" m="0.00560322" t="2.4927"/>\r
63 <eng-data cg="48." f="0." m="0." t="2.5152"/>\r
64 </data>\r
65 </engine>\r
66  </engine-list>\r
67 </engine-database>\r