User Story #916: Hyperion Hinge (Traditional) Concept Generation - CUBICS - AlbertaSat

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User Story #916

closed

Phase #715: Phase B: Preliminary Design and Technology Completion Activities

Epic #977: Preliminary Designs and ICDs

Feature #1032: Preliminary Design: Hinges

Feature #819: Phase B - Deployable Research and Design

Hyperion Hinge (Traditional) Concept Generation

Added by Ben Harbarenko over 1 year ago. Updated over 1 year ago.

Status:

Closed

Priority:

Normal

Assignee:

Sarah Keats

Start date:

10/16/2023

Due date:

11/14/2023

% Done:

Estimated time:

15:00 h

Spent time:

3:40 h

Subsystem:

Mechanical

Success Criteria:

Design parameters established, preliminary concept generated, document everything!

Description

Responsible: Sarah, Alice, Katrina
Accountable: Ben
Consulted: Ben, Mike
Informed: Tyler, Ben

What: Quantifiably establish design parameters for a traditional Hyperion hinge. Refer to the NRCSD-E (https://nanoracks.com/wp-content/uploads/Nanoracks-External-Cygnus-Deployer-E-NRCSD-IDD.pdf) page 13 for the volume envelope available for the satellite. Refer to Ex-Alta 2 CAD as the assumed structure the hinges will interface with (https://drive.google.com/drive/folders/1zw0Y4LhD7IkPOgsIkOr8FfsBMZjpWSua). Generate a preliminary hinge deign that satisfies the design parameters.

Why: It is crucial that a traditional hinge design is prepared for integration of the satellite as it is currently assumed that this will be the design that flies.