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Requirement

Reason

Verification

Party Components

To achieve the goal of a fun rocket with lights and music

Test

Internal Power

To be independent from avionics

Design

Removable Bulkhead

To be able to place components in payload at launch

Design

URRG Requirements

Describe what an external organization (probably ESRA, URRG, or EH&S) requires of this one.

Requirement

Reason

Verification

All components of the rocket must be recovered, and no part of the rocket can be intentionally ballistic

URRG Safety

Analysis

Interface Requirements

Describe what other subsystems require of this one.

Source(s)

Requirement

Reason

Verification

Design

This should describe high-level distinguishing features of this subsystem. If this project is recurring (Space Race or IREC), focus on the items you judge would be important to tell the next year's team, especially specific improvements over previous years.

Post-mortem

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Structures

Polycarb inner diameter of 3.5 in and outer diameter of 4 in

To stay within design constraints given.

Design

Design

The Payload of the FLDSMDFR contains several delicate electronic components contained within a polycarbonate section of tube. Going from the bottom up these components are: a speaker, a camera, fairy lights. In between the speaker and cameral there is a centering ring (originally designed to be a bulkhead with a door on it) that does not allow the camera to fall onto the speaker.

Post-mortem

Despite the overall breakup of the rocket, all electronic components of the payload survived the launch. The speaker is heavily damaged and its buttons no longer work as intended, but it is still able to play sound and continues to be able to pull said audio from the SD card inside. The camera has residue on its lens, but is otherwise completely operational. The fairy lights are fully operational. The payload as a whole worked as intended despite a severely off-nominal launch.


Avionics

Avionics Requirements

Mission Requirements

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