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A supportability simulation for the ...

Cassibry, Phillip J.

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A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster./
作者:	Cassibry, Phillip J.
面頁冊數:	99 p.
附註:	Source: Masters Abstracts International, Volume: 43-05, page: 1803.
Contained By:	Masters Abstracts International43-05.
標題:	Engineering, System Science. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1425529
ISBN:	0496988018

A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster.
Cassibry, Phillip J.

A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster. - 99 p.

Source: Masters Abstracts International, Volume: 43-05, page: 1803.

Thesis (M.S.)--The University of Alabama in Huntsville, 2005.

This study's purpose was to develop a simulation model to determine the adequacy of the finite populations of the re-useable Forward and Aft Integrated Electronics Assemblies (FIEA and AIEA) in the Space Transportation System Solid Rocket Booster to support a 20-year operational life extension. Flight rate (4, 6 flights per year) and refurbishment times (triangular, exponential distributions) were the cases studied for both components. The FIEA population was 99.22% successful in meeting all demands at the lower flight rate over the 20-year study period. The high flight rate resulted in an 18.75% success rate. The AIEA inventory was 12.5% successful at the low flight rate and 0% successful at the high flight rate. Mathematical equations for the AIEA high flight rate cases were developed. More detailed refurbishment time data is needed to further refine this simulation.

ISBN: 0496988018Subjects--Topical Terms:

1018128
Engineering, System Science.

A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster.
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245 1 2 $a A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster.
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500 $a Source: Masters Abstracts International, Volume: 43-05, page: 1803.
500 $a Chair: Phil Farrington.
502 $a Thesis (M.S.)--The University of Alabama in Huntsville, 2005.
520 $a This study's purpose was to develop a simulation model to determine the adequacy of the finite populations of the re-useable Forward and Aft Integrated Electronics Assemblies (FIEA and AIEA) in the Space Transportation System Solid Rocket Booster to support a 20-year operational life extension. Flight rate (4, 6 flights per year) and refurbishment times (triangular, exponential distributions) were the cases studied for both components. The FIEA population was 99.22% successful in meeting all demands at the lower flight rate over the 20-year study period. The high flight rate resulted in an 18.75% success rate. The AIEA inventory was 12.5% successful at the low flight rate and 0% successful at the high flight rate. Mathematical equations for the AIEA high flight rate cases were developed. More detailed refurbishment time data is needed to further refine this simulation.
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