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 language | English |
|---|---|
| Title of host publication | AIAA Aerospace Sciences Meeting |
| DOIs | |
| State | Published - 2018 |
| Event | AIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States Duration: Jan 8 2018 → Jan 12 2018 |
Publication series
| Name | AIAA Aerospace Sciences Meeting, 2018 |
|---|
Conference
| Conference | AIAA Aerospace Sciences Meeting, 2018 |
|---|---|
| Country/Territory | United States |
| City | Kissimmee |
| Period | 1/8/18 → 1/12/18 |
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.
| Funders | Funder number |
|---|---|
| Kentucky EPSCoR NLI | |
| NASA Kentucky Space | |
| NASA USIP SFRO NNX16AI90A | USIP SFRO NNX16AI90A |
| National Aeronautics and Space Administration | NNX13AN04A, NNX15AR69H, NNX16AI90A |
| National Aeronautics and Space Administration |
ASJC Scopus subject areas
- Aerospace Engineering
Fingerprint
Dive into the research topics of 'Overview of the first test-flight of the kentucky re-entry universal payload system (KRUPS)'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver