Space Lithium‐Ion Cells

Borthomieu, Yannick; Smart, Marshall C.; Thwaite, Sara; Bugga, Ratnakumar V.; Barrera, Thomas P.

doi:10.1002/9781119772170.ch2

Cited by 2 publications

(3 citation statements)

References 43 publications

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“…The conversion of force to work will be examined in the sections following magnet design evaluation and must be modelled in component level detail in further research. As the cargo is at rest on the top layer, it's initial velocity is zero, giving a change from zero kinetic energy to a nal kinetic energy of: (10) To achieve the requisite force and e ciently transform stored electrical energy to magnetic then kinetic energy, Nb 3 Sn high energy pulse solenoids, also known as kicker magnets, are ideal and will now be detailed in a review of current literature.…”

Section: 25smentioning

confidence: 99%

“…Today, more than 98% of newly produced satellites are powered by Li-ion [11]. The proposed satellites power system will be based on Li-ion capacitors [10] which are industry standard due to their low cost and high reliability. Two con gurations are proposed by Li-ion suppliers for use in satellite systems: Series-Parallel (S-P) or Parallel-Series (P-S).…”

Section: High Energy Pulsed Solenoidsmentioning

confidence: 99%

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Concept analysis of a distributed thrust system, a novel induction propulsion method using high energy pulse solenoids in satellite swarms for reusable interorbital freight transport.

Wegener¹

2023

Preprint

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To date only single vehicle thrust designs have been considered for propulsion in space, however there is no limitation preventing multivehicle distributed thrust application designs. By considering the regularity of planetary orbits and distance between orbital paths, a location in space can be targeted for next orbit arrival of a shipping container propelled on an intercepting vector that is a result of induction propulsion vector combination. This concept is achieved with Nb3Sn high energy pulse solenoids that enable a square pyramidal swarm of satellites to decompose the intercepting orbital transfer vector and propel a 20 tonne steel shipping container towards a destination swarm. This paper is a thought experiment with first pass mechanical analysis that establishes a validity algorithm then concludes that the proposed yoked solenoid design is fit for purpose and the concept is theoretically functional. The launch vector is perpendicular to the swarm’s orbital path thus force application, reaction and orbital maintenance strategies are investigated. A yoke rod’s enhancement of a superconductive solenoid’s force output and the reaction force distribution model are noted as key variances that must be investigated in further research with numerical modelling tools before the proposed design can be considered fully functional and viable for experimental testing. This design is a dedicated freight transport solution to high mass, high volume cargo required by future astronauts, such as construction machinery and materials.

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Section: 25smentioning

confidence: 99%

Section: High Energy Pulsed Solenoidsmentioning

confidence: 99%

Concept analysis of a distributed thrust system, a novel induction propulsion method using high energy pulse solenoids in satellite swarms for reusable interorbital freight transport.

Wegener¹

2023

Preprint

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“…This way, correlations between the parameters that most influence aging and the chemical changes that take place at the electrode level were found. Given a defined mission and a specific SAFT battery, SLIM can provide reliable RUL prediction [37]. Since this model is specifically for SAFT products, it cannot be applied to satellites with different batteries.…”

Section: Spacementioning

confidence: 99%

Contribution to a review of lithium-ion batteries diagnostic methods for space applications

Chapel,

Picot,

Lacressonniere

et al. 2023

2023 IEEE 14th International Symposium on Diagnostics for Electrical Machines, Power Electronics and Drives (SDEMPED)

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Space Lithium‐Ion Cells

Cited by 2 publications

References 43 publications

Concept analysis of a distributed thrust system, a novel induction propulsion method using high energy pulse solenoids in satellite swarms for reusable interorbital freight transport.

Concept analysis of a distributed thrust system, a novel induction propulsion method using high energy pulse solenoids in satellite swarms for reusable interorbital freight transport.

Contribution to a review of lithium-ion batteries diagnostic methods for space applications

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