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Overview of the first test-flight of the kentucky re-entry universal payload system (KRUPS)

  • J. Devin Sparks
  • , Evan C. Whitmer
  • , Gabriel I. Myers
  • , Courtney C. Montague
  • , Collin J. Dietz
  • , Nicola Khouri
  • , J. Tyler Nichols
  • , Sean C. Field
  • , Suzanne W. Smith
  • , Alexandre Martin

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

14 Scopus citations

Abstract

The design of an efficient Thermal Protection System (TPS) remains one of the most challenging tasks of planetary exploration missions. Because of the harshness of atmospheric entry environments, ground tests cannot replicate these conditions. Consequently, engineers must rely on numerical models that often lack validation data. To provide a path toward inexpensive validation, the Kentucky Reentry Universal Payload System (KRUPS) spacecraft is being developed at the University of Kentucky. As a technology maturation step toward this overall goal, several KRUPS capsules are to be released from sub-orbital flights. In August 2017, a sub-scale version of the KRUPS capsule was successfully ejected at 150 km of altitude, from a sub-orbital sounding rocket. The goal of this first launch was to raise the Technical Readiness Level (TRL) to TRL 6 by demonstrating data acquisition, communication, sensing, and TPS design. The capsule re-entered the atmosphere, and successfully established communication with satellites. However, no data packet was transmitted. This first launch was nevertheless deemed a success, and paved the way for the next series of full scale missions.

Original languageEnglish
Title of host publicationAIAA Aerospace Sciences Meeting
DOIs
StatePublished - 2018
EventAIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States
Duration: Jan 8 2018Jan 12 2018

Publication series

NameAIAA Aerospace Sciences Meeting, 2018

Conference

ConferenceAIAA Aerospace Sciences Meeting, 2018
Country/TerritoryUnited States
CityKissimmee
Period1/8/181/12/18

Bibliographical note

Publisher Copyright:
© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Funding

Financial support for this work was provided by the Kentucky EPSCoR and NASA Award NNX13AN04A, NASA Kentucky Space Grant NNX15AR69H, and NASA USIP SFRO NNX16AI90A. The authors would like to thank F. Taylor, J. Owen, A. Kerr, J. Lumpp, J. Cooper, C. Meek and O. Schroeder of the University of Kentucky, as well as A. Howard and C. Koehler from the University of Colorado for their help with this project. The authors are also immensely thankful to S. Wade at Yokohama, who graciously facilitated the vibration testing.

FundersFunder number
Kentucky EPSCoR NLI
NASA Kentucky Space
NASA USIP SFRO NNX16AI90AUSIP SFRO NNX16AI90A
National Aeronautics and Space AdministrationNNX13AN04A, NNX15AR69H, NNX16AI90A
National Aeronautics and Space Administration

    ASJC Scopus subject areas

    • Aerospace Engineering

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