version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Apogee_1_2A2.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="82.98" Itot="1.221" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1.938" burn-time="0.63" cgDiv="10" cgFix="1" cgStep="-1." code="1/2A2" delays="2,4,6" dia="11." exitDia="0." initWt="4.4" len="57." mDiv="10" mFix="1" mStep="-1." massFrac="34.09" mfg="Apogee" peakThrust="3.97" propWt="1.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4   <comments>Apogee 1/2A2 RASP.ENG file made from NAR published data\r
5 File produced September 4, 2000\r
6 The total impulse, peak thrust, average thrust and burn time are\r
7 the same as the averaged static test data on the NAR web site in\r
8 the certification file. The curve drawn with these data points is as\r
9 close to the certification curve as can be with such a limited\r
10 number of points (32) allowed with wRASP up to v1.6.\r
11 </comments>\r
12   <data>\r
13     <eng-data cg="28.5" f="0." m="1.5" t="0."/>\r
14     <eng-data cg="28.5" f="0.19" m="1.49918" t="0.007"/>\r
15     <eng-data cg="28.5" f="1.494" m="1.45986" t="0.045"/>\r
16     <eng-data cg="28.5" f="3.152" m="1.36566" t="0.078"/>\r
17     <eng-data cg="28.5" f="3.805" m="1.32291" t="0.088"/>\r
18     <eng-data cg="28.5" f="3.805" m="1.29954" t="0.093"/>\r
19     <eng-data cg="28.5" f="3.97" m="1.2661" t="0.1"/>\r
20     <eng-data cg="28.5" f="3.696" m="1.24254" t="0.105"/>\r
21     <eng-data cg="28.5" f="3.071" m="1.22176" t="0.11"/>\r
22     <eng-data cg="28.5" f="2.554" m="1.19756" t="0.117"/>\r
23     <eng-data cg="28.5" f="2.582" m="1.17863" t="0.123"/>\r
24     <eng-data cg="28.5" f="2.31" m="1.15158" t="0.132"/>\r
25     <eng-data cg="28.5" f="2.146" m="1.0667" t="0.163"/>\r
26     <eng-data cg="28.5" f="1.984" m="0.972809" t="0.2"/>\r
27     <eng-data cg="28.5" f="1.902" m="0.872527" t="0.242"/>\r
28     <eng-data cg="28.5" f="2.01" m="0.846087" t="0.253"/>\r
29     <eng-data cg="28.5" f="1.929" m="0.792841" t="0.275"/>\r
30     <eng-data cg="28.5" f="1.929" m="0.63402" t="0.342"/>\r
31     <eng-data cg="28.5" f="1.929" m="0.489421" t="0.403"/>\r
32     <eng-data cg="28.5" f="1.848" m="0.473176" t="0.41"/>\r
33     <eng-data cg="28.5" f="1.902" m="0.450135" t="0.42"/>\r
34     <eng-data cg="28.5" f="1.902" m="0.340282" t="0.467"/>\r
35     <eng-data cg="28.5" f="1.929" m="0.196695" t="0.528"/>\r
36     <eng-data cg="28.5" f="1.929" m="0.108988" t="0.565"/>\r
37     <eng-data cg="28.5" f="1.902" m="0.0736794" t="0.58"/>\r
38     <eng-data cg="28.5" f="1.848" m="0.0437259" t="0.593"/>\r
39     <eng-data cg="28.5" f="1.657" m="0.0221902" t="0.603"/>\r
40     <eng-data cg="28.5" f="1.141" m="0.0101559" t="0.61"/>\r
41     <eng-data cg="28.5" f="0.597" m="0.00481652" t="0.615"/>\r
42     <eng-data cg="28.5" f="0.244" m="0.00119937" t="0.622"/>\r
43     <eng-data cg="28.5" f="0." m="-0." t="0.63"/>\r
44   </data>\r
45 </engine>\r
46  </engine-list>\r
47 </engine-database>\r