3 <engine mfg="Kosdon-by-Aerotech" code="I170S" Type="reloadable" dia="38." len="258."
\r
4 initWt="520." propWt="181.9" delays="14" auto-calc-mass="1" auto-calc-cg="1"
\r
5 avgThrust="175.585" peakThrust="209.199" throatDia="0." exitDia="0."
\r
6 Itot="373.995" burn-time="2.13" massFrac="34.98" Isp="209.66" tDiv="10"
\r
7 tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."
\r
8 mFix="1" cgDiv="10" cgStep="-1." cgFix="1">
\r
9 <comments>Data entered by Tim Van Milligan
\r
10 Based on TRA Certification 6-19-2002
\r
11 And Instructions provided by Aerotech.
\r
14 <eng-data t="0." f="0." m="181.9" cg="129."/>
\r
15 <eng-data t="0.019" f="194.885" m="181." cg="129."/>
\r
16 <eng-data t="0.131" f="190.481" m="170.503" cg="129."/>
\r
17 <eng-data t="0.255" f="191.582" m="158.982" cg="129."/>
\r
18 <eng-data t="0.513" f="199.289" m="134.458" cg="129."/>
\r
19 <eng-data t="0.641" f="204.794" m="121.88" cg="129."/>
\r
20 <eng-data t="0.753" f="206.996" m="110.664" cg="129."/>
\r
21 <eng-data t="0.88" f="209.199" m="97.8105" cg="129."/>
\r
22 <eng-data t="1." f="208.098" m="85.6328" cg="129."/>
\r
23 <eng-data t="1.051" f="208.098" m="80.471" cg="129."/>
\r
24 <eng-data t="1.147" f="206.996" m="70.7803" cg="129."/>
\r
25 <eng-data t="1.24" f="201.491" m="61.5419" cg="129."/>
\r
26 <eng-data t="1.391" f="198.188" m="46.8653" cg="129."/>
\r
27 <eng-data t="1.537" f="190.481" m="33.0656" cg="129."/>
\r
28 <eng-data t="1.707" f="181.672" m="17.6803" cg="129."/>
\r
29 <eng-data t="1.746" f="178.369" m="14.2656" cg="129."/>
\r
30 <eng-data t="1.781" f="173.96" m="11.2667" cg="129."/>
\r
31 <eng-data t="1.808" f="168.46" m="9.01839" cg="129."/>
\r
32 <eng-data t="1.854" f="132.12" m="5.65595" cg="129."/>
\r
33 <eng-data t="1.939" f="53.951" m="1.80973" cg="129."/>
\r
34 <eng-data t="2.005" f="22.02" m="0.590381" cg="129."/>
\r
35 <eng-data t="2.059" f="9.909" m="0.17109" cg="129."/>
\r
36 <eng-data t="2.13" f="0." m="0." cg="129."/>
\r