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Method for calculating aerodynamic heating on sounding rocket tangent ogive noses.

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Bibliographic Details
Title: Method for calculating aerodynamic heating on sounding rocket tangent ogive noses.
Authors: Wing, L. D.
Source: Journal of Spacecraft & Rockets; June 1974, Vol. 11, p357-362, 6p
Database: Applied Science & Technology Source
FullText Text:
  Availability: 0
Header DbId: aci
DbLabel: Applied Science & Technology Source
An: 516730613
AccessLevel: 2
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 0
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  Data: Method for calculating aerodynamic heating on sounding rocket tangent ogive noses.
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  Data: <searchLink fieldCode="AU" term="%22Wing%2C+L%2E+D%2E%22">Wing, L. D.</searchLink>
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RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.2514/3.62081
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 6
        StartPage: 357
    Titles:
      – TitleFull: Method for calculating aerodynamic heating on sounding rocket tangent ogive noses.
        Type: main
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      – PersonEntity:
          Name:
            NameFull: Wing, L. D.
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      – BibEntity:
          Dates:
            – D: 01
              M: 06
              Text: June 1974
              Type: published
              Y: 1974
          Identifiers:
            – Type: issn-print
              Value: 00224650
          Numbering:
            – Type: volume
              Value: 11
          Titles:
            – TitleFull: Journal of Spacecraft & Rockets
              Type: main
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