User Story #915: Compliant Mechanism Concept Generation - CUBICS - AlbertaSat

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User Story #915

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

Compliant Mechanism Concept Generation

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

Status:

Closed

Priority:

Normal

Assignee:

Saksham Verma

Start date:

10/16/2023

Due date:

11/14/2023

% Done:

Estimated time:

30:00 h

Subsystem:

Mechanical

Success Criteria:

Design parameters established, 4 preliminary concepts generated, document everything!

Description

Responsible: Saksham, Jack, Ethan, Brandon, Aryan, Daniel
Accountable: Ben
Consulted: Ben, Mike
Informed: Tyler, Ben

What: Quantifiably establish design parameters for a compliant 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 4 preliminary compliant hinge deigns that satisfy the design parameters.

Why: If CAN RGX is successful in its proposal to SEDS we will be responsible for providing feasible hinge designs for testing. The timeline will be relatively short (they fly in August). So we must get the ball rolling on this task.

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Updated by Ben Harbarenko over 1 year ago

Success Criteria changed from Design parameters established, 4 preliminary concepts generated to Design parameters established, 4 preliminary concepts generated, document everything!

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