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Electronics Design for Krepe Atmosph...

Ruffner, Matt,

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Electronics Design for Krepe Atmospheric Entry Capsule Avionics /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Electronics Design for Krepe Atmospheric Entry Capsule Avionics // Matt Ruffner.
Author:	Ruffner, Matt,
Description:	1 electronic resource (123 pages)
Notes:	Source: Dissertations Abstracts International, Volume: 86-04, Section: A.
Contained By:	Dissertations Abstracts International86-04A.
Subject:	Global positioning systems--GPS. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31607745
ISBN:	9798342146050

Electronics Design for Krepe Atmospheric Entry Capsule Avionics /
Ruffner, Matt,

Electronics Design for Krepe Atmospheric Entry Capsule Avionics /Matt Ruffner. - 1 electronic resource (123 pages)

Source: Dissertations Abstracts International, Volume: 86-04, Section: A.

This research documents the design, testing, and implementation of sensing, control, and communications subsystems for small atmospheric entry capsules. Atmospheric entry capsules pose a unique electronics design challenge given mission requirements, environmental constraints, and inherent risk involved in space based missions. Previous work on small satellites developed the CubeSat platform as a means of ensuring reliability after university-led small satellite missions experienced failures. The publication of the CubeSat platform allowed researchers to focus on the payload science utilizing a standardized form-factor and reusable electronics. Environmental and operational constraints of CubeSats and atmospheric entry capsules overlap and best-practices associated with building CubeSats are applicable to re-entry capsules, however, the limited number of instrumented atmospheric entry experiments yields sparsely published work on their design and testing methodologies. Systems engineering methodologies previously documented with respect to CubeSats are applied in this work to develop, test, and validate atmospheric entry capsules. Considerations include balancing battery capacity and available internal physical space, optimizing scientific data transmission in a low-bandwidth environment, decreasing measurement error in sensing subsystems, and reducing power consumption of dormant electronics. Electronic hardware, software, integration, and testing procedures are presented for three iterations of designs which were validated and improved through four missions.

English

ISBN: 9798342146050Subjects--Topical Terms:

3559357
Global positioning systems--GPS.

Electronics Design for Krepe Atmospheric Entry Capsule Avionics /
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500 $a Advisors: Lumpp, James; Martin, Alexandre.
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520 $a This research documents the design, testing, and implementation of sensing, control, and communications subsystems for small atmospheric entry capsules. Atmospheric entry capsules pose a unique electronics design challenge given mission requirements, environmental constraints, and inherent risk involved in space based missions. Previous work on small satellites developed the CubeSat platform as a means of ensuring reliability after university-led small satellite missions experienced failures. The publication of the CubeSat platform allowed researchers to focus on the payload science utilizing a standardized form-factor and reusable electronics. Environmental and operational constraints of CubeSats and atmospheric entry capsules overlap and best-practices associated with building CubeSats are applicable to re-entry capsules, however, the limited number of instrumented atmospheric entry experiments yields sparsely published work on their design and testing methodologies. Systems engineering methodologies previously documented with respect to CubeSats are applied in this work to develop, test, and validate atmospheric entry capsules. Considerations include balancing battery capacity and available internal physical space, optimizing scientific data transmission in a low-bandwidth environment, decreasing measurement error in sensing subsystems, and reducing power consumption of dormant electronics. Electronic hardware, software, integration, and testing procedures are presented for three iterations of designs which were validated and improved through four missions.
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650 4 $a Software. $2 gtt. $3 619355
650 4 $a Accelerometers. $3 2132687
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720 1 $a Lumpp, James $e degree supervisor.
720 1 $a Martin, Alexandre $e degree supervisor.
773 0 $t Dissertations Abstracts International $g 86-04A.
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