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@JoePfeiffer JoePfeiffer commented Aug 9, 2024

This adds three new stage separation options: separate at a given altitude (ascending), separate at apogee, and separate at a given altitude (descending). All three can have a delay following the trigger event.

Separate at apogee and separate at altitude (descending) are to support deployable payloads, which descend on their own recovery system separate from the rest of the rocket. Separate at altitude (ascending) is to support a conventional booster/sustainer; I noticed recently that at least one flight computer (Altus Metrum EasyMega/TeleMega) can be programmed to fire an event in this circumstance.

Created an example rocket consisting of the existing Simple Model Rocket example with an added deployable payload.

One last thing while I was in there I reordered the fields for recovery device deployment to make the decision flow more obvious; the delay after the triggering event is now the last thing in that dialog.

Fixes #852 and fixes #2519

@SiboVG
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SiboVG commented Aug 9, 2024

Very nice!

@JoePfeiffer JoePfeiffer changed the title Add more stage separation for deployable payloads and a deployable payload example Add more stage separation optionsfor deployable payloads and a deployable payload example Aug 11, 2024
@JoePfeiffer JoePfeiffer changed the title Add more stage separation optionsfor deployable payloads and a deployable payload example Add more stage separation options for deployable payloads and a deployable payload example Aug 11, 2024
@JoePfeiffer JoePfeiffer merged commit 1d13bdc into openrocket:unstable Aug 12, 2024
@JoePfeiffer JoePfeiffer deleted the fix-852 branch August 12, 2024 23:54
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Add an example design that demonstrates payload separation Add more stage separation options

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