In-Situ Turbulence and Particulate Measurements in Support of the BOLT II Flight Experiment

  • Dale A. Lawrence
  • , Brian M. Argrow
  • , Joseph Pointer
  • , Christopher Roseman
  • , Nicholas Kenny
  • , Joseph Habeck
  • , James Flaten
  • , Graham V. Candler
  • , Aroh Barjatya
  • , Julio Guardado

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

The results of a measurement campaign to characterize the freestream atmospheric turbulence intensity and particulate concentrations experienced by the Boundary Layer Transition (BOLT) II flight experiment are described. These measurements were obtained using custom high-altitude balloon-borne payloads using a modified commercial optical particle counter and a high-bandwidth coldwire thermometer and hotwire anemometer, designed for low cost and light weight, with telemetered data so that physical payload recovery is not necessary. Sixteen flights were carried out over a 10-day campaign, with viable data returned from 14 flights, including four centered on the BOLT II launch with 1-h cadence. Turbulence and particulate measurements are shown vs altitude for all 14 data sets, along with statistics derived from the measurements, quantifying the BOLT II atmospheric environment for use in assessing the impact of these freestream disturbances on the hypersonic-vehicle boundary layer.

Original languageEnglish (US)
Pages (from-to)1563-1576
Number of pages14
JournalJournal of Spacecraft and Rockets
Volume61
Issue number6
DOIs
StatePublished - 2024

Bibliographical note

Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Keywords

  • Aerodynamics
  • Atmospheric Environment
  • Atmospheric Turbulence
  • High Altitude Balloon
  • Hotwire Anemometry
  • Hypersonic Boundary Layer Transition
  • Hypersonic Flows
  • Hypersonic Vehicles
  • Orbital Property
  • Thermometers

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