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Record W3200525348 · doi:10.32393/csme.2021.239

Radsat-SK Cube-Satellite Frame Design

2021· article· en· W3200525348 on OpenAlexaffabout
Brendon Entz, Daniel Franko, Seamus Woodward-George, Atharva Parag Kulkarni, Alexandra Hynes, Spencer Bast, Addi Amaya, Sean Maw, Christoper A Amaya

Bibliographic record

VenueProgress in Canadian Mechanical Engineering. Volume 4 · 2021
Typearticle
Languageen
FieldEngineering
TopicSpacecraft Design and Technology
Canadian institutionsUniversity of Saskatchewan
Fundersnot available
KeywordsCube (algebra)Computer scienceSatelliteFrame (networking)Computer graphics (images)TelecommunicationsEngineeringMathematicsAerospace engineeringGeometry

Abstract

fetched live from OpenAlex

This abstract outlines the custom frame design for Saskatchewan's first Cubesat, the RADSAT-SK. The justification behind a custom frame design was the enhancement of student education and the ability to cater to the specific needs of RADSAT-SK's mission. Payload preservation and the mounting of the solar assembly are essential to the success of this cube-satellite mission. Therefore, the frame must incorporate many intricate aspects including structural stability, thermal survivability, and accessibility. The frame must securely anchor all components of the cubesat during launch while minimizing the effects of mission vibrations, remaining accessible for all pre-launch work, and facilitating radiation conduction when in orbit. The RADSAT-SK's custom frame design is the implementation of a repeating, modular L-shaped design that combines a shear panel and rail for each side of the cube-satellite into one contiguous bracket. This design takes advantage of strategically placed ribs to reduce the fastener count, such that each L-bracket is easily removed for access to the internal payload by the removal of four (4) fasteners. This permits inspection and testing of the payload without complete disassembly of the cubesat. The payload bus is secured to the frame by three (3) cross members and can be removed from the cubesat in one piece. This provides stability for the payload while simplifying disassembly during pre-launch procedures. The RADSAT-SK frame design simplifies secondary component integration, reduces the frame's mass and component count, and improves clearances. The frame meets the Nanoracks integration requirements, ensuring the frame is compatible with the designated deployment mechanism from the International Space Station (ISS). Aluminum (6061-T6) was chosen as the material for the frame's fabrication due to a history of being successfully employed in aerospace applications. Thermal and vibration simulation tests were conducted to confirm design viability using Siemens NX and ANSYS software packages, respectively. For thermal control, the simulations showed that the cubesat frame will not require any additional heat management mechanisms. Regarding vibrations, the frame adheres to GSFC-STD-7000 and ASAP5 qualifications. The frame will undergo a series of physical tests to validate the vibrational analyses performed through simulations, using a hydrostatic-bearing slip table. Likewise, the custom-built frame will be tested in a thermal vacuum chamber to ensure its ability to conduct radiation to maintain desired internal temperatures. The RADSAT-SK frame is uniquely designed and optimized for the team's mission to ensure its structural integrity.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesMeta-epidemiology (narrow)
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: none
Teacher disagreement score0.891
Threshold uncertainty score1.000

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.001
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0010.001
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.009
GPT teacher head0.201
Teacher spread0.191 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one teacher head, not a consensus.

Study designSimulation or modeling
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations0
Published2021
Admission routes2
Has abstractyes

Explore more

Same venueProgress in Canadian Mechanical Engineering. Volume 4Same topicSpacecraft Design and TechnologyFrench-language works237,207