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A supportability simulation for the ...
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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.
Record Type:
Electronic resources : Monograph/item
Title/Author:
A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster./
Author:
Cassibry, Phillip J.
Description:
99 p.
Notes:
Source: Masters Abstracts International, Volume: 43-05, page: 1803.
Contained By:
Masters Abstracts International43-05.
Subject:
Engineering, System Science. -
Online resource:
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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A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster.
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99 p.
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Source: Masters Abstracts International, Volume: 43-05, page: 1803.
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Chair: Phil Farrington.
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Thesis (M.S.)--The University of Alabama in Huntsville, 2005.
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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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http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1425529
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