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  • Other Sources  (2)
  • 1990-1994  (1)
  • 1985-1989  (1)
  • 1955-1959
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  • 1990-1994  (1)
  • 1985-1989  (1)
  • 1955-1959
  • 1965-1969  (2)
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  • 1
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    Unknown
    End-mass instrumentation for the first SEDS/Delta II mission (1990)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The dynamics instrumentation is described which will be flown in the end-mass of the first tethered satellite to be deployed from a Delta II launch vehicle with the SEDS (Small Expendable Deployer System) low-tension deployer. Transducers, signal conditioning, power supply design, data acquisition procedures and data recovery plans are discussed. The effects of temperature variations and other potential error sources are considered.
    Keywords: SPACECRAFT INSTRUMENTATION
    Type: AIAA PAPER 90-0537
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 2
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    Continuous, Multielement, Hot-Film Transition Gage (1986)
    In:  Other Sources
    Details
    Publication Date: 2019-07-12
    Description: Accurate measurement of location where laminar boundary layer undergoes transition to turbulent one serves many purposes in basic aero-dynamic research and developmental testing. Individual gages must be staggered to prevent formation of turbulence at gages downstream. This arrangement precludes accurate measurements of laminar/turbulent transition regions along streamline. Complete understanding of performance, stability, and control of laminar-flow airplane requires knowledge of transition locations on wing surface, empennage surfaces, fuselage, and nacelles. Visual, acoustic, and electronic methods capable of providing this transition information.
    Keywords: MECHANICS
    Type: LAR-13319 , NASA Tech Briefs (ISSN 0145-319X); 10; 3; P. 97
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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