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Record W69420310

The Canadian Advanced Nanospace eXperiment 7 (CanX-7) Demonstration Mission: De-Orbiting Nano- and Microspacecraft

2012· article· en· W69420310 on OpenAlexfundaboutno aff
Barbara Shmuel, Jesse Hiemstra, Vincent Tarantini, Fiona Singarayar, Grant Bonin, Robert Zee

Bibliographic record

VenueDigital Commons - USU (Utah State University) · 2012
Typearticle
Languageen
FieldEngineering
TopicSpacecraft Design and Technology
Canadian institutionsnot available
FundersNatural Sciences and Engineering Research Council of Canada
KeywordsCubeSatSatelliteOrbit (dynamics)AeronauticsSpace debrisAerospace engineeringLow earth orbitComputer scienceModular designSpacecraftSystems engineeringRemote sensingEngineeringGeology
DOInot available

Abstract

fetched live from OpenAlex

As the number of objects in Earth orbit grows, the international satellite community faces a growing problem associated with orbital debris and space collision avoidance. In September 2007, the Inter-Agency Space Debris Coordination Committee (IADC) recommended that satellites de-orbit within 25 years after the completion of their mission, or within 30 years of launch if they cannot be parked in less dense (“graveyard”) orbits. Governments around the world are introducing procedures to implement the recommendations of the IADC, and consequently, this requirement poses a significant programmatic risk for new space missions, especially those requiring rapid, responsive, short missions in low Earth orbit. Unfortunately for nano- and microsatellites—which are ideally suited for responsive, short missions—no mature de orbiting technology currently exists that is suitable for a wide range of missions and orbits. The CanX-7 (Canadian Advanced Nanosatellite eXperiment-7) mission aims to accomplish a successful demonstration of a low-cost, passive nano- and microsatellite de-orbiting device. Currently under development at the University of Toronto’s Space Flight Laboratory, CanX-7 will employ a lightweight, compact, modular deployable drag sail to de-orbit a demonstrator nanosatellite. The sail design is highly compact, and a variant of this sail can fit onto even the smallest “cubesat”-based platforms. In order to facilitate acceptance and use by the industry, the sail is specifically designed to be minimally intrusive to the operational mission of the hosting satellite. CanX-7 will demonstrate the drag sail’s ability to meet the requirements of the IADC and enable future missions to proceed without delays. A summary of the CanX-7 mission is presented along with the lifetime analysis and innovative features of the sail that make it attractive to future missions – missions that need de-orbiting assistance but that are sensitive to the risk and resource requirements associated with incorporating a de-orbiting device.

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 machine prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. The Gemma side is a direct model label for every work in the frame, read from the title-only record. The Codex side is a classifier learned from the 10,348 direct Codex labels and calibrated to design-weighted sample rates; fields without enough sample support carry no Codex call. Candidate is the union of the two sides; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels.

metaresearch head score (Codex)0.001
metaresearch head score (Gemma)0.000
Version: metacan-v3-hybrid-931329e0061cValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.736
Threshold uncertainty score0.526

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0010.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0020.001
Scholarly communication0.0010.001
Open science0.0010.001
Research integrity0.0010.001
Insufficient payload (model declined to judge)0.0020.001

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 head0.191
Teacher spread0.182 · 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 source (direct Gemma or distilled Codex), not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designBench or experimental
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

Citations10
Published2012
Admission routes2
Has abstractyes

Explore more

Same venueDigital Commons - USU (Utah State University)Same topicSpacecraft Design and TechnologyFrench-language works237,207