Add more stage separation options for deployable payloads and a deployable payload example #2529
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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