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Issue #53: team-02 - Openrocket Integration #109

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Issue #53: team-02 - Openrocket Integration #109

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beaf152
Created initial ork import testing
smkinney979 Aug 28, 2022
9f81841
Updated utilities file for .ork functions
smkinney979 Aug 28, 2022
9c1e150
Removed unnecessary files
smkinney979 Aug 28, 2022
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283 changes: 283 additions & 0 deletions data/lazarus/lazarus-uncompressed/rocket.ork
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<?xml version='1.0' encoding='utf-8'?>
<openrocket version="1.4" creator="OpenRocket 15.03">
<rocket>
<name>Rocket</name>
<motorconfiguration configid="bcb82022-f301-40de-8cae-e068b6c72e12"/>
<motorconfiguration configid="c872ec37-7f90-437c-9a46-d85ae9c25680"/>
<motorconfiguration configid="45097303-41ec-4952-8480-1aec9cbb95cd" default="true"/>
<referencetype>maximum</referencetype>

<subcomponents>
<stage>
<name>Sustainer</name>
<overridemass>24.757071532768</overridemass>
<overridecg>2.3114</overridecg>
<overridesubcomponents>true</overridesubcomponents>

<subcomponents>
<nosecone>
<name>Nose cone</name>
<overridemass>1.612</overridemass>
<overridesubcomponents>false</overridesubcomponents>
<finish>smooth</finish>
<material type="bulk" density="680.0">Cardboard</material>
<length>0.6687312</length>
<thickness>0.002</thickness>
<shape>haack</shape>
<shapeclipped>false</shapeclipped>
<shapeparameter>0.0</shapeparameter>
<aftradius>0.11137899999999999</aftradius>
<aftshoulderradius>0.0</aftshoulderradius>
<aftshoulderlength>0.0</aftshoulderlength>
<aftshoulderthickness>0.0</aftshoulderthickness>
<aftshouldercapped>false</aftshouldercapped>
</nosecone>

<bodytube>
<name>Fin Can</name>
<overridemass>3.056</overridemass>
<overridesubcomponents>false</overridesubcomponents>
<finish>smooth</finish>
<material type="bulk" density="680.0">Cardboard</material>
<length>3.2258</length>
<thickness>0.002</thickness>
<radius>auto</radius>
<motormount>
<ignitionevent>automatic</ignitionevent>
<ignitiondelay>0.0</ignitiondelay>
<overhang>0.0</overhang>
<motor configid="bcb82022-f301-40de-8cae-e068b6c72e12">
<manufacturer>TAMUSRT</manufacturer>
<digest>78c3a4a99e8a9f23471d80cde35aa4ac</digest>
<designation>N27</designation>
<diameter>0.0577</diameter>
<length>2.2918000000000003</length>
<delay>none</delay>
</motor>
<motor configid="c872ec37-7f90-437c-9a46-d85ae9c25680">
<manufacturer>TAMUSRT-30k</manufacturer>
<digest>61987aa8d66e09e7e9842c644c1ee006</digest>
<designation>N27-30k</designation>
<diameter>0.0577</diameter>
<length>2.2918000000000003</length>
<delay>none</delay>
</motor>
<motor configid="45097303-41ec-4952-8480-1aec9cbb95cd">
<manufacturer>AeroTech</manufacturer>
<digest>f097ce447c4666d6124670f2768d667a</digest>
<designation>N2000W</designation>
<diameter>0.098</diameter>
<length>1.046</length>
<delay>0.0</delay>
</motor>
</motormount>

<subcomponents>
<trapezoidfinset>
<name>Trapezoidal fin set</name>
<position type="absolute">3.4798</position>
<finish>smooth</finish>
<material type="bulk" density="680.0">Cardboard</material>
<fincount>3</fincount>
<rotation>0.0</rotation>
<thickness>0.0254</thickness>
<crosssection>airfoil</crosssection>
<cant>0.0</cant>
<filletradius>0.0</filletradius>
<filletmaterial type="bulk" density="680.0">Cardboard</filletmaterial>
<rootchord>0.30479999999999996</rootchord>
<tipchord>0.07619999999999999</tipchord>
<sweeplength>0.22352</sweeplength>
<height>0.2794</height>
</trapezoidfinset>

<parachute>
<name>Drogue</name>
<position type="top">0.0</position>
<packedlength>0.025</packedlength>
<packedradius>0.0125</packedradius>
<radialposition>0.0</radialposition>
<radialdirection>0.0</radialdirection>
<cd>2.2</cd>
<material type="surface" density="0.067">Ripstop nylon</material>
<deployevent>apogee</deployevent>
<deployaltitude>200.0</deployaltitude>
<deploydelay>1.0</deploydelay>
<diameter>2.032</diameter>
<linecount>6</linecount>
<linelength>0.3</linelength>
<linematerial type="line" density="0.0018">Elastic cord (round 2 mm, 1/16 in)</linematerial>
</parachute>

<parachute>
<name>Main</name>
<position type="top">0.0</position>
<packedlength>0.025</packedlength>
<packedradius>0.0125</packedradius>
<radialposition>0.0</radialposition>
<radialdirection>0.0</radialdirection>
<cd>auto</cd>
<material type="surface" density="0.067">Ripstop nylon</material>
<deployevent>altitude</deployevent>
<deployaltitude>304.8</deployaltitude>
<deploydelay>0.0</deploydelay>
<diameter>0.3</diameter>
<linecount>6</linecount>
<linelength>0.3</linelength>
<linematerial type="line" density="0.0018">Elastic cord (round 2 mm, 1/16 in)</linematerial>
</parachute>
</subcomponents>
</bodytube>

<transition>
<name>Transition</name>
<finish>smooth</finish>
<material type="bulk" density="680.0">Cardboard</material>
<length>0.23622</length>
<thickness>0.002</thickness>
<shape>ellipsoid</shape>
<shapeclipped>true</shapeclipped>
<foreradius>auto</foreradius>
<aftradius>0.073152</aftradius>
<foreshoulderradius>0.0</foreshoulderradius>
<foreshoulderlength>0.0</foreshoulderlength>
<foreshoulderthickness>0.0</foreshoulderthickness>
<foreshouldercapped>false</foreshouldercapped>
<aftshoulderradius>0.0</aftshoulderradius>
<aftshoulderlength>0.0</aftshoulderlength>
<aftshoulderthickness>0.0</aftshoulderthickness>
<aftshouldercapped>false</aftshouldercapped>
</transition>
</subcomponents>
</stage>
</subcomponents>
</rocket>

<simulations>
<simulation status="notsimulated">
<name>Simulation 1</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>bcb82022-f301-40de-8cae-e068b6c72e12</configid>
<launchrodlength>1.0</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
</simulation>

<simulation status="outdated">
<name>Simulation 2</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>bcb82022-f301-40de-8cae-e068b6c72e12</configid>
<launchrodlength>1.0</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
<flightdata maxaltitude="2759.2" maxvelocity="209.47" maxacceleration="44.007" maxmach="0.62029" timetoapogee="26.051" flighttime="123.6" groundhitvelocity="60.133" launchrodvelocity="9.161">
</flightdata>
</simulation>

<simulation status="notsimulated">
<name>Simulation 3</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>c872ec37-7f90-437c-9a46-d85ae9c25680</configid>
<launchrodlength>1.0</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
</simulation>

<simulation status="outdated">
<name>Simulation 4</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>c872ec37-7f90-437c-9a46-d85ae9c25680</configid>
<launchrodlength>1.0</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
<flightdata maxaltitude="5856.3" maxvelocity="316.52" maxacceleration="35.436" maxmach="0.95758" timetoapogee="38.171" flighttime="175.45" groundhitvelocity="38.07" launchrodvelocity="8.2438">
</flightdata>
</simulation>

<simulation status="outdated">
<name>Simulation 5</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>c872ec37-7f90-437c-9a46-d85ae9c25680</configid>
<launchrodlength>9.144</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
<flightdata maxaltitude="5948.1" maxvelocity="321.45" maxacceleration="36.461" maxmach="0.9731" timetoapogee="38.201" flighttime="178.87" groundhitvelocity="37.532" launchrodvelocity="25.649">
</flightdata>
</simulation>

<simulation status="notsimulated">
<name>Simulation 6</name>
<simulator>RK4Simulator</simulator>
<calculator>BarrowmanCalculator</calculator>
<conditions>
<configid>45097303-41ec-4952-8480-1aec9cbb95cd</configid>
<launchrodlength>1.0</launchrodlength>
<launchrodangle>0.0</launchrodangle>
<launchroddirection>90.0</launchroddirection>
<windaverage>2.0</windaverage>
<windturbulence>0.1</windturbulence>
<launchaltitude>0.0</launchaltitude>
<launchlatitude>28.61</launchlatitude>
<launchlongitude>-80.6</launchlongitude>
<geodeticmethod>spherical</geodeticmethod>
<atmosphere model="isa"/>
<timestep>0.05</timestep>
</conditions>
</simulation>
</simulations>
</openrocket>
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