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data/thrustcurve.org/AeroTech/C3_5f4294d20002e90000000800.eng

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+; Aerotech C3.4-PT RASP.ENG file made from NAR published data
+; File produced, 2013
+; The total impulse, peak thrust, average thrust and burn time are
+; the same as the averaged static test data on the NAR web site in
+; the certification file. The curve drawn with these data points is as
+; close to the certification curve as can be with such a limited
+; number of points (32) allowed with wRASP up to v1.6.
+C3.4 18 72 0 .0052 .0239 A
+0.023 3.188
+0.028 5.669
+0.093 9.080
+0.235 8.208
+0.427 6.881
+0.513 6.188
+0.600 5.438
+0.666 4.803
+0.762 3.649
+0.838 2.668
+0.970 2.149
+1.228 1.918
+1.522 1.918
+1.800 1.860
+2.013 1.745
+2.068 2.034
+2.134 1.803
+2.326 1.803
+2.509 1.745
+2.645 1.687
+2.721 1.457
+2.807 0.879
+2.860 0.000

data/thrustcurve.org/AeroTech/C3_5f923f0a1bca5800041716ae.rse

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+<engine-database>
+  <engine-list>
+    <engine  mfg="Aerotech" code="C3.4" Type="single-use" dia="18." len="72." initWt="23.9"
+propWt="5.2" delays="0" auto-calc-mass="1" auto-calc-cg="1" avgThrust="3.133"
+peakThrust="9.08" throatDia="0." exitDia="0." Itot="8.959" burn-time="2.86"
+massFrac="21.76" Isp="175.69" tDiv="10" tStep="-1." tFix="1" FDiv="10"
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
+cgFix="1">
+    <comments>Aerotech C3.4-PT RASP.ENG file made from NAR published data
+File produced, 2013
+The total impulse, peak thrust, average thrust and burn time are
+the same as the averaged static test data on the NAR web site in
+the certification file. The curve drawn with these data points is as
+close to the certification curve as can be with such a limited
+number of points (32) allowed with wRASP up to v1.6.
+</comments>
+    <data>
+      <eng-data  t="0." f="0." m="5.2" cg="36."/>
+      <eng-data  t="0.023" f="3.188" m="5.17872" cg="36."/>
+      <eng-data  t="0.028" f="5.669" m="5.16587" cg="36."/>
+      <eng-data  t="0.093" f="9.08" m="4.88765" cg="36."/>
+      <eng-data  t="0.235" f="8.208" m="4.17521" cg="36."/>
+      <eng-data  t="0.427" f="6.881" m="3.33445" cg="36."/>
+      <eng-data  t="0.513" f="6.188" m="3.00827" cg="36."/>
+      <eng-data  t="0.6" f="5.438" m="2.71473" cg="36."/>
+      <eng-data  t="0.666" f="4.803" m="2.51858" cg="36."/>
+      <eng-data  t="0.762" f="3.649" m="2.2831" cg="36."/>
+      <eng-data  t="0.838" f="2.668" m="2.14377" cg="36."/>
+      <eng-data  t="0.97" f="2.149" m="1.95925" cg="36."/>
+      <eng-data  t="1.228" f="1.918" m="1.65473" cg="36."/>
+      <eng-data  t="1.522" f="1.918" m="1.32744" cg="36."/>
+      <eng-data  t="1.8" f="1.86" m="1.02263" cg="36."/>
+      <eng-data  t="2.013" f="1.745" m="0.799792" cg="36."/>
+      <eng-data  t="2.068" f="2.034" m="0.739473" cg="36."/>
+      <eng-data  t="2.134" f="1.803" m="0.665979" cg="36."/>
+      <eng-data  t="2.326" f="1.803" m="0.465052" cg="36."/>
+      <eng-data  t="2.509" f="1.745" m="0.276623" cg="36."/>
+      <eng-data  t="2.645" f="1.687" m="0.141166" cg="36."/>
+      <eng-data  t="2.721" f="1.457" m="0.0718222" cg="36."/>
+      <eng-data  t="2.807" f="0.879" m="0.01352" cg="36."/>
+      <eng-data  t="2.86" f="0." m="0." cg="36."/>
+    </data>
+  </engine>
+</engine-list>
+</engine-database>

data/thrustcurve.org/AeroTech/D10_5f4294d20002e9000000067b.eng

@@ -0,0 +1,24 @@
+D10 18 70 7 0.009800000000000001 0.0259 AT
+   0.0070 23.0
+   0.018 25.0
+   0.027 20.25
+   0.066 20.25
+   0.073 18.5
+   0.094 20.25
+   0.112 20.75
+   0.137 19.75
+   0.163 21.5
+   0.202 20.75
+   0.231 20.75
+   0.254 22.75
+   0.27 20.75
+   0.504 20.0
+   0.536 18.25
+   0.607 17.0
+   0.687 14.75
+   0.751 14.25
+   0.84 11.25
+   0.998 8.25
+   1.024 8.25
+   1.248 2.5
+   1.385 0.0

data/thrustcurve.org/AeroTech/D10_5f923f481bca5800041716b3.rse

@@ -0,0 +1,37 @@
+<engine-database>
+  <engine-list>
+    <engine  mfg="Aerotech" code="D10" Type="single-use" dia="18." len="70." initWt="25.9"
+propWt="9.8" delays="7" auto-calc-mass="1" auto-calc-cg="1" avgThrust="13.473"
+peakThrust="25." throatDia="0." exitDia="0." Itot="18.66" burn-time="1.39"
+massFrac="37.84" Isp="194.16" tDiv="10" tStep="-1." tFix="1" FDiv="10"
+FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10" cgStep="-1."
+cgFix="1">
+    <data>
+      <eng-data  t="0." f="0." m="9.8" cg="35."/>
+      <eng-data  t="0.007" f="23." m="9.75772" cg="35."/>
+      <eng-data  t="0.018" f="25." m="9.61907" cg="35."/>
+      <eng-data  t="0.027" f="20.25" m="9.51213" cg="35."/>
+      <eng-data  t="0.066" f="20.25" m="9.09736" cg="35."/>
+      <eng-data  t="0.073" f="18.5" m="9.02613" cg="35."/>
+      <eng-data  t="0.094" f="20.25" m="8.81244" cg="35."/>
+      <eng-data  t="0.112" f="20.75" m="8.61865" cg="35."/>
+      <eng-data  t="0.137" f="19.75" m="8.35277" cg="35."/>
+      <eng-data  t="0.163" f="21.5" m="8.07114" cg="35."/>
+      <eng-data  t="0.202" f="20.75" m="7.63844" cg="35."/>
+      <eng-data  t="0.231" f="20.75" m="7.32241" cg="35."/>
+      <eng-data  t="0.254" f="22.75" m="7.05968" cg="35."/>
+      <eng-data  t="0.27" f="20.75" m="6.87692" cg="35."/>
+      <eng-data  t="0.504" f="20." m="4.37294" cg="35."/>
+      <eng-data  t="0.536" f="18.25" m="4.05152" cg="35."/>
+      <eng-data  t="0.607" f="17." m="3.39431" cg="35."/>
+      <eng-data  t="0.687" f="14.75" m="2.72732" cg="35."/>
+      <eng-data  t="0.751" f="14.25" m="2.23994" cg="35."/>
+      <eng-data  t="0.84" f="11.25" m="1.64398" cg="35."/>
+      <eng-data  t="0.998" f="8.25" m="0.834923" cg="35."/>
+      <eng-data  t="1.024" f="8.25" m="0.722269" cg="35."/>
+      <eng-data  t="1.248" f="2.5" m="0.089939" cg="35."/>
+      <eng-data  t="1.385" f="0." m="0." cg="35."/>
+    </data>
+  </engine>
+</engine-list>
+</engine-database>

data/thrustcurve.org/AeroTech/D13_5f4294d20002e9000000027c.eng

@@ -0,0 +1,40 @@
+; Aerotech D13 RASP.ENG file made from NAR published data
+; File produced July 4, 2000
+; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
+; The total impulse, peak thrust, average thrust and burn time are
+; the same as the averaged static test data on the NAR web site in
+; the certification file. The curve drawn with these data points is as
+; close to the certification curve as can be with such a limited
+; number of points (32) allowed with wRASP up to v1.6.
+D13W   18   70   4-7-10   0.0098   0.0326 AT
+   0.030   13.462
+   0.061   21.171
+   0.085   20.618
+   0.127   21.605
+   0.158   21.042
+   0.182   22.306
+   0.217   22.592
+   0.227   23.610
+   0.248   21.891
+   0.279   23.155
+   0.317   22.039
+   0.366   21.338
+   0.383   21.901
+   0.449   20.648
+   0.462   21.486
+   0.480   19.947
+   0.507   19.947
+   0.521   20.509
+   0.559   18.693
+   0.580   19.118
+   0.660   17.578
+   0.743   15.337
+   0.861   12.406
+   0.947    9.329
+   1.068    5.834
+   1.155    4.158
+   1.172    4.720
+   1.231    2.762
+   1.328    1.928
+   1.404    1.093
+   1.520    0.000

data/thrustcurve.org/AeroTech/D13_5f4294d20002e90000000379.rse

@@ -0,0 +1,16 @@
+<engine-database>
+ <engine-list>
+<engine FDiv="10" FFix="1" FStep="-1." Isp="199.6" Itot="19.183" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="11.284" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="D13" delays="4,7,10" dia="18." exitDia="0." initWt="33." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="29.7" mfg="Aerotech" peakThrust="22.25" propWt="9.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
+  <data>
+    <eng-data cg="35." f="0." m="9.8" t="0."/>
+    <eng-data cg="35." f="22.25" m="9.74317" t="0.01"/>
+    <eng-data cg="35." f="22.25" m="7.58344" t="0.2"/>
+    <eng-data cg="35." f="20." m="5.42499" t="0.4"/>
+    <eng-data cg="35." f="12.5" m="2.1043" t="0.8"/>
+    <eng-data cg="35." f="8." m="1.057" t="1."/>
+    <eng-data cg="35." f="1.34" m="0.102686" t="1.4"/>
+    <eng-data cg="35." f="0." m="0." t="1.7"/>
+  </data>
+</engine>
+ </engine-list>
+</engine-database>

data/thrustcurve.org/AeroTech/D15_5f4294d20002e9000000027b.eng

@@ -0,0 +1,26 @@
+; Aerotech D15 RASP.ENG file made from NAR published data
+; File produced July 4, 2000
+; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
+; The total impulse, peak thrust, average thrust and burn time are
+; the same as the averaged static test data on the NAR web site in
+; the certification file. The curve drawn with these data points is as
+; close to the certification curve as can be with such a limited
+; number of points (32) allowed with wRASP up to v1.6.
+D15T  24   70   4-6-8   .0089   .0440   AT
+   0.014   11.480
+   0.049   26.272
+   0.081   30.087
+   0.107   31.261
+   0.121   31.249
+   0.159   31.360
+   0.208   31.249
+   0.283   29.583
+   0.439   23.353
+   0.551   18.484
+   0.675   13.430
+   0.863    6.422
+   0.938    3.892
+   1.010    2.335
+   1.085    0.778
+   1.142    0.389
+   1.150    0.000

data/thrustcurve.org/AeroTech/D15_5f4294d20002e9000000037a.rse

@@ -0,0 +1,15 @@
+<engine-database>
+ <engine-list>
+<engine FDiv="10" FFix="1" FStep="-1." Isp="224.77" Itot="19.617" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="14.012" burn-time="1.4" cgDiv="10" cgFix="1" cgStep="-1." code="D15" delays="4,6" dia="24." exitDia="0." initWt="44." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="20.23" mfg="Aerotech" peakThrust="28.5" propWt="8.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
+<data>
+  <eng-data cg="35." f="0." m="8.9" t="0."/>
+  <eng-data cg="35." f="26." m="8.84102" t="0.01"/>
+  <eng-data cg="35." f="28.5" m="7.72838" t="0.1"/>
+  <eng-data cg="35." f="23." m="4.22373" t="0.4"/>
+  <eng-data cg="35." f="11.2" m="1.12058" t="0.8"/>
+  <eng-data cg="35." f="4.5" m="0.408309" t="1."/>
+  <eng-data cg="35." f="0." m="0." t="1.4"/>
+</data>
+</engine>
+ </engine-list>
+</engine-database>