43 lines
1.9 KiB
Plaintext
43 lines
1.9 KiB
Plaintext
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The current OpenRocket file format is "documented" only as the
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reference implementation. This will hopefully change in the future.
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The "version" attribute of the <openrocket> tag describes the file
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format version used, while the "creator" attribute MAY describe the
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software and version used to write the document.
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The file format version is increased every time the format is
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changed. The minor number is increased when changes are made that are
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mostly backward-compatible, meaning that older software versions
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should be able to read the design sans the new features. The major
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number is increased when changes are made that render the design
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problematic or impossible to read for older software. For maximum
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compatibility software should save a file in the oldest file format
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version that supports all the necessary design features.
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The following file format versions exist:
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1.0: File format version of the first public release (OpenRocket 0.9.0)
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1.1: Introduced with OpenRocket 0.9.4. Adds support for saving fin
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tabs (<tabheight>, <tablength> and <tabposition> elements) and
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allows attaching subcomponents to a tube coupler (previously
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forbidden).
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1.2: Introduced with OpenRocket 1.1.1. Adds the <digest> tag to
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motor definitions. The digest uniquely identifies the
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functional characteristics of a particular thrust curve motor.
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1.3: Introduced with OpenRocket 1.1.9. Adds the <launchlongitude> and
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<geodeticmethod> parameters to the simulation conditions element.
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1.4: Introduced with OpenRocket 12.03. Adds the launchrodvelocity and
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deploymentvelocity attributes to <flightdata> element. The motor
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digesting algorithm was changed. Adds <separationevent> and
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<separationdelay> elements to stage components (except sustainer).
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1.5: Introduced with OpenRocket 12.xx. Added ComponentPresets.
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Added lowerstageseparation as recovery device deployment event. |