Difference between revisions of "RSE File"

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(Add (partial) list of XML fields / tags within an RSE file; added example file (AeroTech E18))
(→‎Introduction: changed verbage to better match english.)
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== Introduction  ==
 
== Introduction  ==
  
Also called "RockSim XML format" and using an '.rse" extension, these files are used to describe a motor for entry into Rocksim and OpenRocket.  
+
Also called "RockSim XML format" and using an '.rse" extension, these files are used to describe a motor for loading into Rocksim and OpenRocket.  
  
 
RockSim v8 uses either the RASP or the new RockSim XML format (.rse). The .rse format can store extra information about the motors, such as the type of engine it is (single-use, reloadable, hybrid).  
 
RockSim v8 uses either the RASP or the new RockSim XML format (.rse). The .rse format can store extra information about the motors, such as the type of engine it is (single-use, reloadable, hybrid).  
  
 
For more information about entering motor information into Rocksim, please also read the FAQ entry: [http://wiki.openrocket.info/FAQ/en#How_do_I_define_motors.3F]
 
For more information about entering motor information into Rocksim, please also read the FAQ entry: [http://wiki.openrocket.info/FAQ/en#How_do_I_define_motors.3F]
 
  
 
== XML Tags ==
 
== XML Tags ==

Revision as of 23:52, 15 October 2014


Introduction

Also called "RockSim XML format" and using an '.rse" extension, these files are used to describe a motor for loading into Rocksim and OpenRocket.

RockSim v8 uses either the RASP or the new RockSim XML format (.rse). The .rse format can store extra information about the motors, such as the type of engine it is (single-use, reloadable, hybrid).

For more information about entering motor information into Rocksim, please also read the FAQ entry: [1]

XML Tags

Engine Tag Attributes

  • mfg= text string. Manufacturer.
  • code= text string. unknown use.
  • Type= text string. one of : ("single-use" | ? )
  • dia="18.001"
  • len="200."
  • initWt="800."
  • propWt="800."
  • delays="1000"
  • auto-calc-mass="1"
  • auto-calc-cg="0"
  • avgThrust="280.059"
  • peakThrust="428.329"
  • throatDia="0."
  • exitDia="0."
  • Itot="21.284"
  • burn-time="0.08"
  • massFrac="99.88"
  • Isp="2.71"
  • tDiv="10"
  • tStep="-1."
  • tFix="1"
  • FDiv="10"
  • FStep="-1."
  • FFix="1"
  • mDiv="10"
  • mStep="-1."
  • mFix="1" cgDiv="10"
  • cgStep="-1."
  • cgFix="1">

Engine Tag Children

  • comments

String. Text Description

  • data

A list of "eng-data" tags. Together this list will define the thrust curve (and other properties which change over time.

eng-data Tag Attributes

  • time ("t"): number. units = ??
  • force ("f"): number. units = ??
  • mass ("m"): number. units = ??
  • center of gravity location: ("cg"): number. units = ??

Example File

<engine-database>
  <engine-list>
    <engine FDiv="10" FFix="1" FStep="-1." Isp="195.96" Itot="39.78" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1"
    avgThrust="18.082" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="E18" delays="4,8" dia="24." exitDia="0." initWt="57." 
    len="70." mDiv="10" mFix="1" mStep="-1." massFrac="36.32" mfg="Aerotech" peakThrust="31." propWt="20.7" tDiv="10" tFix="1" 
    tStep="-1." throatDia="0.">
      <data>
        <eng-data cg="35." f="0." m="20.7" t="0."/>
        <eng-data cg="35." f="31." m="20.3774" t="0.04"/>
        <eng-data cg="35." f="30." m="14.6638" t="0.4"/>
        <eng-data cg="35." f="26.7" m="8.7629" t="0.8"/>
        <eng-data cg="35." f="19.1" m="3.99638" t="1.2"/>
        <eng-data cg="35." f="8." m="1.17602" t="1.6"/>
        <eng-data cg="35." f="2.2" m="0.11448" t="2."/>
        <eng-data cg="35." f="0." m="0." t="2.2"/>
      </data>
    </engine>
  </engine-list>
</engine-database>