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Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.

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Title: Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.
Authors: Rahimi, Muhammad Fadhli Hairi Abd1, Ariffin, Ahmad Hamdan1, ahmadh@uthm.edu.my
Source: Progress in Aerospace & Aviation Technology (PAAT); 2025, Vol. 5 Issue 2, p8-16, 9p
Database: Applied Science & Technology Source
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  Availability: 0
Header DbId: aci
DbLabel: Applied Science & Technology Source
An: 191671674
AccessLevel: 2
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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  Data: Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.
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PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=aci&AN=191671674
RecordInfo BibRecord:
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      – Type: doi
        Value: 10.30880/paat.2025.05.02.002
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      – Code: eng
        Text: English
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        PageCount: 9
        StartPage: 8
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      – TitleFull: Design and Analysis of Nozzle Exit Area for Science Technology Engineering and Mathematics (STEM) Based Solid Rocket Propellant.
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            NameFull: Rahimi, Muhammad Fadhli Hairi Abd
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            NameFull: Ariffin, Ahmad Hamdan
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            – D: 01
              M: 07
              Text: 2025
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              Y: 2025
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