Design And Testing Of The Electrical Power Subsystem For The Spudnik-1 Cubesat
Open accessAbstract
The EPS is designed to support a CubeSat carrying an optical payload to capture soil and crop data; average power consumption is 2.190 W and average power generation is 2.977 W, with staged testing from subsystem to module to system level.
Integrity signals
Registry
Cites
Statistics
Claims the paper makes
- Findingnone given
With the CubeSat's current components, the average power consumption is 2.190 W.
“With the CubeSat's current components, the average power consumption is 2.190W”
Quote in the paperSubstantial claim - Findingown data
With the CubeSat's current components, the average power generated is 2.977 W.
“the average power generated is 2.977W”
Quote in the paperSubstantial claim
- Classified as probably not a substantial claim. 2
Probably not a substantial claim: may not pass S4 (based).
Interpretationnone givenThe EPS needs to ensure that the battery does not fall under 80% charge throughout the mission to ensure the batteries' longevity and efficiency.
“The EPS also needs to ensure that the battery does not fall under 80% charge throughout the mission to ensure the batteries' longevity and efficiency.”
Quote in the paperNot a substantial claimClassified as probably not a substantial claim.
Interpretationown dataOver the 16 orbits, the EPS should provide sufficient power to all parts of the CubeSat.
“Over the 16 orbits, the EPS should provide sufficient power to all parts of the CubeSat.”
Quote in the paperSubstantial claim
- Authors
- Shokr, O., McCardle, C., Nyong, E., Speelman, T., VanIderstine, N., Bloemink, J., McSorley, G., & Krouglicof, N.
- Affiliations
- University of Prince Edward Island (CA)
- Venue
- Progress in Canadian Mechanical Engineering. Volume 4
- Published
- 2021-06-27
- OpenAlex
- W3199498139
- Cited by
- 0
- References
- 0
- FWCI
- 0.00
- Type
- conference paper
- Language
- en
- Open access
- bronze
- doi.org
- Locations
- Progress in Canadian Mechanical Engineering. Volume 4 (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Energy Harvesting in Wireless Networks
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Advanced DC-DC Converters
- Keywords
- CubeSat, power subsystem, optical payload, agricultural data, agricultural efficiency
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Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
Claims read by deepseek-v4.1-flash under definition version 3 (extract-v3) on 2026-10-10.
Classified by jev-1.13-20260917 (gold-guideline-v0.2) on 2026-10-10.
Statistics and arithmetic are recomputed, not judged.
Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.
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